Abstract

We report the results of video observations of tiny (diameter less than 100 m) near-Earth objects (NEOs) with Tomo-e Gozen on the Kiso 105 cm Schmidt telescope. The rotational period of a tiny asteroid reflects its dynamical history and physical properties since smaller objects are sensitive to the Yarkovsky–O’Keefe–Radzievskii–Paddack (YORP) effect. We carried out video observations of 60 tiny NEOs at 2 fps from 2018 to 2021 and successfully derived the rotational periods and axial ratios of 32 NEOs including 13 fast rotators with rotational periods less than 60 s. The fastest rotator found during our survey is 2020 HS|$_\mathsf {7}$| with a rotational period of 2.99 s. We statistically confirmed that there is a certain number of tiny fast rotators in the NEO population, which have been missed with all previous surveys. We have discovered that the distribution of the tiny NEOs in a diameter and rotational period (D–P) diagram is truncated around a period of 10 s. The truncation with a flat-top shape is not explained well by either a realistic tensile strength of NEOs or the suppression of YORP by meteoroid impacts. We propose that the dependence of the tangential YORP effect on the rotational period potentially explains the observed pattern in the D–P diagram.

1 Introduction

As of 2022 March, 28527 near-Earth objects (NEOs) have been discovered by wide-field monitoring surveys such as the Catalina Sky Survey (CSS; Drake et al. 2009), the Panoramic Survey Telescope and Rapid Response System (Pan-STARRS; Chambers et al. 2016), and the Asteroid Terrestrial-impact Last Alert System (ATLAS; Tonry et al. 2018).1 Most NEOs have their origins in the main belt (e.g., Bottke et al. 2000; Granvik et al. 2018). Asteroidal fragments are generated from collisional events in the main belt and their orbital elements are gradually changed by the Yarkovsky effect, which is a thermal force caused by radiation from the Sun (e.g., Vokrouhlický 1998; Vokrouhlický et al. 2000; Bottke et al. 2006). When the asteroids enter into orbital resonances with giant bodies, their orbits evolve to those of NEOs in a few Myr (e.g., Gladman et al. 1997; Bottke et al. 2006). During the orbital evolution, the rotational states (i.e., rotational period and pole direction) of the object are changed by the Yarkovsky–O’Keefe–Radzievskii–Paddack (YORP) effect, which arises from the asymmetricity of scattered sunlight and thermal radiation from its surface (e.g., Rubincam 2000; Vokrouhlický & Čapek 2002; Čapek & Vokrouhlický 2004; Bottke et al. 2006). The YORP effect caused by a recoil force normal to the surface, NYORP, is investigated intensively in previous studies. Recently, the tangential YORP (TYORP) effect, which is caused by a recoil force parallel to the surface, was proposed by Golubov and Kruguly (2012).

Since the strength of the YORP effect increases with decreasing diameter, smaller asteroids would experience a larger change in the rotational states. Thus, YORP is a dominant mechanism to change the rotational states of kilometer-sized or smaller asteroids (Vokrouhlický & Čapek 2002). The rotational acceleration by YORP leads to deformation or rotational fission of the asteroid due to a strong centrifugal force. Because the YORP strength is also dependent on physical properties such as shape and thermal conductivity, the rotational period distribution of smaller objects probably reflects the dynamical history and physical properties.

In general, it is difficult to constrain the rotational states of tiny asteroids due to limited observational windows (hours to days), fast rotation (less than a minute), and large apparent motion on the sky (a few arcsec s−1). Observations with exposure times sufficiently shorter than their rotational periods are required. The shorter exposure times are effective in suppressing the trailing sensitivity loss effect, which is the degradation of the surface brightness of a moving object on an image (Zhai et al. 2014).

The Asteroid Lightcurve Database (LCDB; Warner et al. 2009) has thousands of rotational periods of minor planets. The diameter and rotational period relation (hereinafter referred to as the D–P relation) is shown in figure 1. As of 2021 June, rotational periods of 5060 objects are estimated with high accuracy [the quality code U in Warner et al. (2009) is 3 or 3-]. For asteroids larger than 200 m in diameter, the rotation period distribution is truncated at around two hours. This clear structure is called the cohesionless spin barrier and indicates that most of the larger asteroids are rubble-piles (Pravec & Harris 2000). It is possible to constrain physical properties of asteroids smaller than 200 m in diameter from the D–P relation in the same way as the larger asteroids. However, there is a smaller number of asteroids for which the rotational period has been reported so far.

Diameter and rotational period relation of the objects in the LCDB (Warner et al. 2009) as of 2021 June. NEOs and other objects (main belt and trans-Neptunian objects) are presented as filled circles and plus signs, respectively. A cohesionless spin barrier assuming a typical density of S-type asteroids of 2.67 g cm−3 (Yeomans et al. 2000) is shown by a dashed line. The tiny (D ≤ 100 m) and fast (P ≤ 10 min) biased region is shown as a gray shaded area.
Fig. 1.

Diameter and rotational period relation of the objects in the LCDB (Warner et al. 2009) as of 2021 June. NEOs and other objects (main belt and trans-Neptunian objects) are presented as filled circles and plus signs, respectively. A cohesionless spin barrier assuming a typical density of S-type asteroids of 2.67 g cm−3 (Yeomans et al. 2000) is shown by a dashed line. The tiny (D ≤ 100 m) and fast (P ≤ 10 min) biased region is shown as a gray shaded area.

The LCDB contains the observational results of the Mission Accessible Near-Earth Objects Survey (MANOS), which obtained more than 300 light curves of small NEOs with the mean absolute magnitude of about 24 mag using large and medium aperture telescopes (Thirouin et al. 2016, 2018). Although MANOS successfully derived the rotational periods of NEOs with high accuracy, the main motivation of the survey is not to detect fast rotators, but to characterize mission-accessible NEOs. Due to a relatively long exposure time (1–300 s), the survey possibly did not detect the very fast rotations. Systematic high-speed observations are required to derive shorter rotational periods correctly and obtain an unbiased D–P relation of tiny NEOs.

In this paper, we report the results of imaging observations at 2 fps of 60 tiny NEOs with the wide-field CMOS camera Tomo-e Gozen. The observed NEOs are smaller than 100 m in diameter and their mean diameter is 20 m. The aims of this study are to obtain an unbiased D–P relation by video observations and to reveal dynamical histories and physical properties of tiny NEOs. Observations and data reduction are described in section 2. The results are compared with previous studies in section 3. In section 4, the D–P relation of the tiny NEOs obtained in this study is discussed taking into account the spin acceleration by YORP.

2 Observations and data reduction

2.1 Observations

We conducted photometric observations at 2 fps with the wide-field CMOS camera Tomo-e Gozen (Sako et al. 2018). Tomo-e Gozen is a wide-field high-speed camera mounted on the 105 cm Schmidt telescope at Kiso Observatory (Minor Planet Center code 381) in Nagano, Japan. The field of view is 20.7 square degrees covered by 84 chips of CMOS sensors without photometric filters. A timestamp of each image data is GPS-synchronized and has a time accuracy of 0.2 ms. We have performed 2 fps all-sky survey observations with Tomo-e Gozen since 2019. Data accumulated each night amount to 30 TB, from which various types of transients such as supernovae and tiny NEOs are searched for. Tomo-e Gozen has discovered 32 NEOs from the survey data in real time from 2019 March to 2021 October with the fast-moving object pipeline using a machine-learning technique (R. Ohsawa et al. in preparation). The algorithms used in the pipeline are partly described in Ohsawa (2021).

We have obtained light curves of 60 NEOs from 2018 May to 2021 October. Nominal criteria for target selection are that the V-band apparent magnitude (V) is smaller than 17 and the absolute magnitude (H) is larger than 22.5. We took V and H from the International Astronomical Union Minor Planet Center website2 to make observation plans. We call our selected samples hereinafter the Tomo-e NEOs, which are listed in table 1. The observation specifications are from NASA JPL/HORIZONS3 with astroquery.jplhorizons (Ginsburg et al. 2019). The Tomo-e NEOs consists of 37 NEOs discovered by other facilities and 23 NEOs discovered by Tomo-e Gozen itself. The V-band magnitude of 17 corresponds to a 5-sigma limiting magnitude in 2 fps video observations with Tomo-e Gozen. The asteroid diameter (D) in table 1 is derived from H using the equation (Fowler & Chillemi 1992; Pravec & Harris 2007):
(1)
where pV is a geometric albedo in theh V band.
Table 1.

Summary of observations.*

ObjectDyn.HDObs. dateTVVel.αΔrNote
class(mag)(m)(UTC)(min)(mag)(arcsec s−1)(°)(au)(au)
2010 WC9Apollo23.5592018-05-15 12:19:0114.012.32.328.00.00331.0138
2011 DWAten22.9792021-02-28 15:15:3620.016.40.510.00.03701.0271
2017 WJ16Aten24.5372020-11-23 17:42:4816.016.70.437.10.01360.9982
2020-11-25 13:30:5960.016.70.334.90.01410.9986
2018 LV3Apollo26.5152018-06-13 15:18:08100.017.90.433.60.00961.02365 s exposure
2018 UD3Apollo26.2172018-11-01 13:47:4636.517.11.050.30.00640.9966
2019 BE5Aten25.1282019-02-01 09:58:47114.017.50.739.10.01460.9967
2020 EOApollo25.9202020-03-13 10:47:0513.016.31.129.60.00660.9998
2020 FA2Apollo27.592020-03-18 16:53:3044.017.41.322.50.00571.0008
2020 FL2Apollo26.1182020-03-22 13:28:4814.014.52.111.70.00351.0001
2020 GY1Apollo26.6142020-04-05 17:16:2814.014.91.324.00.00281.0032
2020 HK3Apollo24.2432020-04-30 13:41:5413.017.21.669.20.01291.0120
2020 HS7Apollo29.142020-04-28 14:36:3114.016.03.019.10.00151.0085
2020-04-28 16:24:419.015.18.425.70.00091.0079
2020 HT7Apollo26.9122020-04-27 16:40:3713.016.91.139.50.00491.0105
2020 HU3Apollo26.0192020-04-21 16:23:066.017.61.332.00.01091.0144
2020 PW2Apollo28.852020-08-14 16:46:4824.017.82.024.80.00371.0162Crowded field
2020 PY2Apollo26.5152020-08-20 12:50:5623.015.72.312.10.00491.0165
2020 QWApollo25.3262020-08-17 16:10:5120.018.30.973.40.01221.0158Crowded field
2020 TD8Apollo26.9122020-10-26 16:59:3517.017.21.048.30.00500.9972
2020 TE6Apollo27.4102020-10-18 10:30:5019.016.83.262.90.00270.9975
2020 TS1Aten29.242020-10-12 10:13:049.016.83.637.40.00170.9993
2020 UQ6Apollo22.7862020-10-28 17:30:3517.016.00.416.00.02971.0219
2020 VF4Apollo26.6142020-11-13 16:56:2320.017.02.018.50.00780.9968
2020 VH5Apollo29.242020-11-13 17:33:0421.015.95.47.70.00170.9912
2020 VJ1Apollo26.7132020-11-09 15:23:3020.016.63.134.10.00490.9944
2020 VR1Apollo28.952020-11-09 15:44:3716.017.56.436.10.00260.9925
2020 VZ6Apollo25.0302020-12-02 14:07:0214.014.71.131.00.00490.9900
2020 XHApollo24.6362020-12-05 16:35:3917.016.80.624.20.01651.0004Crowded field
2020 XH1Apollo22.9782020-12-08 12:56:0920.016.70.430.90.03021.0108
2020 XQ2Apollo22.8832020-12-09 15:00:3920.016.60.815.00.03931.0228
2020 XX3Apollo28.562020-12-17 14:09:5218.016.51.038.00.00200.9856
2020 XY4Aten26.9122020-12-20 11:10:5120.017.32.140.30.00590.9883Thin cloud
2020 YJ2Apollo27.4102020-12-21 14:09:0920.016.72.335.70.00390.9869Crowded field
2021 AT5Apollo27.592021-01-13 13:40:0910.016.91.817.90.00500.9884Crowded field
2021 BCAten24.3412021-01-21 10:55:3518.015.91.855.70.00830.9888
2021 CA6Apollo28.562021-02-13 16:03:0422.016.08.166.30.00110.9879
2021 CC7Apollo29.832021-02-12 18:06:5811.017.12.611.50.00210.9894
2021 CGApollo26.1182021-02-06 15:18:4120.017.01.116.70.00980.9957
2021 COApollo25.3262021-02-09 12:12:0521.016.60.27.30.01431.0009
2021 DW1Apollo25.2272021-03-02 11:14:222.016.20.549.20.00700.9957Crowded field
2021 EM4Apollo27.1112021-03-18 16:04:3720.016.81.526.60.00500.9999
2021 EQ3Apollo26.1182021-03-15 11:07:0314.016.61.049.60.00530.9980
2021 ET4Apollo23.9482021-03-16 14:20:1718.017.00.745.10.01841.0078
2021 EX1Apollo24.9322021-03-08 12:53:1120.016.90.522.30.01531.0069
2021 FHApollo26.7132021-03-22 13:13:5120.017.30.321.50.00801.0040Thin cloud
2021 GD5Aten27.1112021-04-08 15:38:3620.018.22.724.30.00981.0104
2021 GQ10Apollo26.6142021-04-14 16:03:0220.015.42.865.70.00201.0040
2021 GT3Apollo26.4162021-04-10 13:03:3220.015.72.111.50.00521.0071
2021 JB6Apollo28.852021-05-13 15:11:1020.016.82.747.30.00171.0118
2021 KN2Apollo28.662021-05-30 16:53:2914.017.12.341.20.00231.0156
2021 KQ2Aten29.932021-05-31 16:27:1020.017.22.939.10.00141.0150
2021 RB1Amor24.1462021-09-06 13:16:1020.016.81.126.50.01991.0258
2021 RX5Apollo23.7542021-09-15 15:25:567.016.60.533.20.01961.0219
2021 TG1Apollo28.272021-10-03 13:22:3220.017.12.539.40.00291.0028
2021 TL14Apollo26.9122021-10-14 14:45:0021.015.72.427.80.00331.0004
2021 TQ3Atira27.1112021-10-06 16:25:1120.017.11.421.30.00621.0055
2021 TQ4Apollo29.932021-10-06 16:54:273.017.33.12.40.00261.0023
2021 TY14Apollo27.2112021-10-15 11:56:3920.017.01.822.20.00561.0023
2021 UF12Apollo29.342021-10-29 14:46:188.016.59.214.00.00190.9951
TMG0042Apollo28.562021-04-10 16:16:1720.0NEO candidate
TMG0049Apollo30.032021-05-30 15:30:0916.0NEO candidate
ObjectDyn.HDObs. dateTVVel.αΔrNote
class(mag)(m)(UTC)(min)(mag)(arcsec s−1)(°)(au)(au)
2010 WC9Apollo23.5592018-05-15 12:19:0114.012.32.328.00.00331.0138
2011 DWAten22.9792021-02-28 15:15:3620.016.40.510.00.03701.0271
2017 WJ16Aten24.5372020-11-23 17:42:4816.016.70.437.10.01360.9982
2020-11-25 13:30:5960.016.70.334.90.01410.9986
2018 LV3Apollo26.5152018-06-13 15:18:08100.017.90.433.60.00961.02365 s exposure
2018 UD3Apollo26.2172018-11-01 13:47:4636.517.11.050.30.00640.9966
2019 BE5Aten25.1282019-02-01 09:58:47114.017.50.739.10.01460.9967
2020 EOApollo25.9202020-03-13 10:47:0513.016.31.129.60.00660.9998
2020 FA2Apollo27.592020-03-18 16:53:3044.017.41.322.50.00571.0008
2020 FL2Apollo26.1182020-03-22 13:28:4814.014.52.111.70.00351.0001
2020 GY1Apollo26.6142020-04-05 17:16:2814.014.91.324.00.00281.0032
2020 HK3Apollo24.2432020-04-30 13:41:5413.017.21.669.20.01291.0120
2020 HS7Apollo29.142020-04-28 14:36:3114.016.03.019.10.00151.0085
2020-04-28 16:24:419.015.18.425.70.00091.0079
2020 HT7Apollo26.9122020-04-27 16:40:3713.016.91.139.50.00491.0105
2020 HU3Apollo26.0192020-04-21 16:23:066.017.61.332.00.01091.0144
2020 PW2Apollo28.852020-08-14 16:46:4824.017.82.024.80.00371.0162Crowded field
2020 PY2Apollo26.5152020-08-20 12:50:5623.015.72.312.10.00491.0165
2020 QWApollo25.3262020-08-17 16:10:5120.018.30.973.40.01221.0158Crowded field
2020 TD8Apollo26.9122020-10-26 16:59:3517.017.21.048.30.00500.9972
2020 TE6Apollo27.4102020-10-18 10:30:5019.016.83.262.90.00270.9975
2020 TS1Aten29.242020-10-12 10:13:049.016.83.637.40.00170.9993
2020 UQ6Apollo22.7862020-10-28 17:30:3517.016.00.416.00.02971.0219
2020 VF4Apollo26.6142020-11-13 16:56:2320.017.02.018.50.00780.9968
2020 VH5Apollo29.242020-11-13 17:33:0421.015.95.47.70.00170.9912
2020 VJ1Apollo26.7132020-11-09 15:23:3020.016.63.134.10.00490.9944
2020 VR1Apollo28.952020-11-09 15:44:3716.017.56.436.10.00260.9925
2020 VZ6Apollo25.0302020-12-02 14:07:0214.014.71.131.00.00490.9900
2020 XHApollo24.6362020-12-05 16:35:3917.016.80.624.20.01651.0004Crowded field
2020 XH1Apollo22.9782020-12-08 12:56:0920.016.70.430.90.03021.0108
2020 XQ2Apollo22.8832020-12-09 15:00:3920.016.60.815.00.03931.0228
2020 XX3Apollo28.562020-12-17 14:09:5218.016.51.038.00.00200.9856
2020 XY4Aten26.9122020-12-20 11:10:5120.017.32.140.30.00590.9883Thin cloud
2020 YJ2Apollo27.4102020-12-21 14:09:0920.016.72.335.70.00390.9869Crowded field
2021 AT5Apollo27.592021-01-13 13:40:0910.016.91.817.90.00500.9884Crowded field
2021 BCAten24.3412021-01-21 10:55:3518.015.91.855.70.00830.9888
2021 CA6Apollo28.562021-02-13 16:03:0422.016.08.166.30.00110.9879
2021 CC7Apollo29.832021-02-12 18:06:5811.017.12.611.50.00210.9894
2021 CGApollo26.1182021-02-06 15:18:4120.017.01.116.70.00980.9957
2021 COApollo25.3262021-02-09 12:12:0521.016.60.27.30.01431.0009
2021 DW1Apollo25.2272021-03-02 11:14:222.016.20.549.20.00700.9957Crowded field
2021 EM4Apollo27.1112021-03-18 16:04:3720.016.81.526.60.00500.9999
2021 EQ3Apollo26.1182021-03-15 11:07:0314.016.61.049.60.00530.9980
2021 ET4Apollo23.9482021-03-16 14:20:1718.017.00.745.10.01841.0078
2021 EX1Apollo24.9322021-03-08 12:53:1120.016.90.522.30.01531.0069
2021 FHApollo26.7132021-03-22 13:13:5120.017.30.321.50.00801.0040Thin cloud
2021 GD5Aten27.1112021-04-08 15:38:3620.018.22.724.30.00981.0104
2021 GQ10Apollo26.6142021-04-14 16:03:0220.015.42.865.70.00201.0040
2021 GT3Apollo26.4162021-04-10 13:03:3220.015.72.111.50.00521.0071
2021 JB6Apollo28.852021-05-13 15:11:1020.016.82.747.30.00171.0118
2021 KN2Apollo28.662021-05-30 16:53:2914.017.12.341.20.00231.0156
2021 KQ2Aten29.932021-05-31 16:27:1020.017.22.939.10.00141.0150
2021 RB1Amor24.1462021-09-06 13:16:1020.016.81.126.50.01991.0258
2021 RX5Apollo23.7542021-09-15 15:25:567.016.60.533.20.01961.0219
2021 TG1Apollo28.272021-10-03 13:22:3220.017.12.539.40.00291.0028
2021 TL14Apollo26.9122021-10-14 14:45:0021.015.72.427.80.00331.0004
2021 TQ3Atira27.1112021-10-06 16:25:1120.017.11.421.30.00621.0055
2021 TQ4Apollo29.932021-10-06 16:54:273.017.33.12.40.00261.0023
2021 TY14Apollo27.2112021-10-15 11:56:3920.017.01.822.20.00561.0023
2021 UF12Apollo29.342021-10-29 14:46:188.016.59.214.00.00190.9951
TMG0042Apollo28.562021-04-10 16:16:1720.0NEO candidate
TMG0049Apollo30.032021-05-30 15:30:0916.0NEO candidate
*

Dynamical class (Dyn. class) and absolute magnitude (H) are from NASA JPL/HORIZONS as of 2022-1-9 (UTC). Observation starting time in UTC (Obs. date) and duration time of observation (T) for each object are listed. V-band apparent magnitude (V), angular rate of change in apparent RA and Dec (Vel.), phase angle (α), distance between NEO and observer (Δ), and distance between Sun and NEO (r) at the observation time are also from NASA JPL/HORIZONS as of 2022-1-9 (UTC).

Diameter (D) is derived from H assuming geometric albedo in V-band of 0.20.

Dyn. class and H of the NEO candidates are derived from orbits determined with the Tomo-e Gozen data using Find_Orb: 〈https://www.projectpluto.com/fo.htm〉.

Table 1.

Summary of observations.*

ObjectDyn.HDObs. dateTVVel.αΔrNote
class(mag)(m)(UTC)(min)(mag)(arcsec s−1)(°)(au)(au)
2010 WC9Apollo23.5592018-05-15 12:19:0114.012.32.328.00.00331.0138
2011 DWAten22.9792021-02-28 15:15:3620.016.40.510.00.03701.0271
2017 WJ16Aten24.5372020-11-23 17:42:4816.016.70.437.10.01360.9982
2020-11-25 13:30:5960.016.70.334.90.01410.9986
2018 LV3Apollo26.5152018-06-13 15:18:08100.017.90.433.60.00961.02365 s exposure
2018 UD3Apollo26.2172018-11-01 13:47:4636.517.11.050.30.00640.9966
2019 BE5Aten25.1282019-02-01 09:58:47114.017.50.739.10.01460.9967
2020 EOApollo25.9202020-03-13 10:47:0513.016.31.129.60.00660.9998
2020 FA2Apollo27.592020-03-18 16:53:3044.017.41.322.50.00571.0008
2020 FL2Apollo26.1182020-03-22 13:28:4814.014.52.111.70.00351.0001
2020 GY1Apollo26.6142020-04-05 17:16:2814.014.91.324.00.00281.0032
2020 HK3Apollo24.2432020-04-30 13:41:5413.017.21.669.20.01291.0120
2020 HS7Apollo29.142020-04-28 14:36:3114.016.03.019.10.00151.0085
2020-04-28 16:24:419.015.18.425.70.00091.0079
2020 HT7Apollo26.9122020-04-27 16:40:3713.016.91.139.50.00491.0105
2020 HU3Apollo26.0192020-04-21 16:23:066.017.61.332.00.01091.0144
2020 PW2Apollo28.852020-08-14 16:46:4824.017.82.024.80.00371.0162Crowded field
2020 PY2Apollo26.5152020-08-20 12:50:5623.015.72.312.10.00491.0165
2020 QWApollo25.3262020-08-17 16:10:5120.018.30.973.40.01221.0158Crowded field
2020 TD8Apollo26.9122020-10-26 16:59:3517.017.21.048.30.00500.9972
2020 TE6Apollo27.4102020-10-18 10:30:5019.016.83.262.90.00270.9975
2020 TS1Aten29.242020-10-12 10:13:049.016.83.637.40.00170.9993
2020 UQ6Apollo22.7862020-10-28 17:30:3517.016.00.416.00.02971.0219
2020 VF4Apollo26.6142020-11-13 16:56:2320.017.02.018.50.00780.9968
2020 VH5Apollo29.242020-11-13 17:33:0421.015.95.47.70.00170.9912
2020 VJ1Apollo26.7132020-11-09 15:23:3020.016.63.134.10.00490.9944
2020 VR1Apollo28.952020-11-09 15:44:3716.017.56.436.10.00260.9925
2020 VZ6Apollo25.0302020-12-02 14:07:0214.014.71.131.00.00490.9900
2020 XHApollo24.6362020-12-05 16:35:3917.016.80.624.20.01651.0004Crowded field
2020 XH1Apollo22.9782020-12-08 12:56:0920.016.70.430.90.03021.0108
2020 XQ2Apollo22.8832020-12-09 15:00:3920.016.60.815.00.03931.0228
2020 XX3Apollo28.562020-12-17 14:09:5218.016.51.038.00.00200.9856
2020 XY4Aten26.9122020-12-20 11:10:5120.017.32.140.30.00590.9883Thin cloud
2020 YJ2Apollo27.4102020-12-21 14:09:0920.016.72.335.70.00390.9869Crowded field
2021 AT5Apollo27.592021-01-13 13:40:0910.016.91.817.90.00500.9884Crowded field
2021 BCAten24.3412021-01-21 10:55:3518.015.91.855.70.00830.9888
2021 CA6Apollo28.562021-02-13 16:03:0422.016.08.166.30.00110.9879
2021 CC7Apollo29.832021-02-12 18:06:5811.017.12.611.50.00210.9894
2021 CGApollo26.1182021-02-06 15:18:4120.017.01.116.70.00980.9957
2021 COApollo25.3262021-02-09 12:12:0521.016.60.27.30.01431.0009
2021 DW1Apollo25.2272021-03-02 11:14:222.016.20.549.20.00700.9957Crowded field
2021 EM4Apollo27.1112021-03-18 16:04:3720.016.81.526.60.00500.9999
2021 EQ3Apollo26.1182021-03-15 11:07:0314.016.61.049.60.00530.9980
2021 ET4Apollo23.9482021-03-16 14:20:1718.017.00.745.10.01841.0078
2021 EX1Apollo24.9322021-03-08 12:53:1120.016.90.522.30.01531.0069
2021 FHApollo26.7132021-03-22 13:13:5120.017.30.321.50.00801.0040Thin cloud
2021 GD5Aten27.1112021-04-08 15:38:3620.018.22.724.30.00981.0104
2021 GQ10Apollo26.6142021-04-14 16:03:0220.015.42.865.70.00201.0040
2021 GT3Apollo26.4162021-04-10 13:03:3220.015.72.111.50.00521.0071
2021 JB6Apollo28.852021-05-13 15:11:1020.016.82.747.30.00171.0118
2021 KN2Apollo28.662021-05-30 16:53:2914.017.12.341.20.00231.0156
2021 KQ2Aten29.932021-05-31 16:27:1020.017.22.939.10.00141.0150
2021 RB1Amor24.1462021-09-06 13:16:1020.016.81.126.50.01991.0258
2021 RX5Apollo23.7542021-09-15 15:25:567.016.60.533.20.01961.0219
2021 TG1Apollo28.272021-10-03 13:22:3220.017.12.539.40.00291.0028
2021 TL14Apollo26.9122021-10-14 14:45:0021.015.72.427.80.00331.0004
2021 TQ3Atira27.1112021-10-06 16:25:1120.017.11.421.30.00621.0055
2021 TQ4Apollo29.932021-10-06 16:54:273.017.33.12.40.00261.0023
2021 TY14Apollo27.2112021-10-15 11:56:3920.017.01.822.20.00561.0023
2021 UF12Apollo29.342021-10-29 14:46:188.016.59.214.00.00190.9951
TMG0042Apollo28.562021-04-10 16:16:1720.0NEO candidate
TMG0049Apollo30.032021-05-30 15:30:0916.0NEO candidate
ObjectDyn.HDObs. dateTVVel.αΔrNote
class(mag)(m)(UTC)(min)(mag)(arcsec s−1)(°)(au)(au)
2010 WC9Apollo23.5592018-05-15 12:19:0114.012.32.328.00.00331.0138
2011 DWAten22.9792021-02-28 15:15:3620.016.40.510.00.03701.0271
2017 WJ16Aten24.5372020-11-23 17:42:4816.016.70.437.10.01360.9982
2020-11-25 13:30:5960.016.70.334.90.01410.9986
2018 LV3Apollo26.5152018-06-13 15:18:08100.017.90.433.60.00961.02365 s exposure
2018 UD3Apollo26.2172018-11-01 13:47:4636.517.11.050.30.00640.9966
2019 BE5Aten25.1282019-02-01 09:58:47114.017.50.739.10.01460.9967
2020 EOApollo25.9202020-03-13 10:47:0513.016.31.129.60.00660.9998
2020 FA2Apollo27.592020-03-18 16:53:3044.017.41.322.50.00571.0008
2020 FL2Apollo26.1182020-03-22 13:28:4814.014.52.111.70.00351.0001
2020 GY1Apollo26.6142020-04-05 17:16:2814.014.91.324.00.00281.0032
2020 HK3Apollo24.2432020-04-30 13:41:5413.017.21.669.20.01291.0120
2020 HS7Apollo29.142020-04-28 14:36:3114.016.03.019.10.00151.0085
2020-04-28 16:24:419.015.18.425.70.00091.0079
2020 HT7Apollo26.9122020-04-27 16:40:3713.016.91.139.50.00491.0105
2020 HU3Apollo26.0192020-04-21 16:23:066.017.61.332.00.01091.0144
2020 PW2Apollo28.852020-08-14 16:46:4824.017.82.024.80.00371.0162Crowded field
2020 PY2Apollo26.5152020-08-20 12:50:5623.015.72.312.10.00491.0165
2020 QWApollo25.3262020-08-17 16:10:5120.018.30.973.40.01221.0158Crowded field
2020 TD8Apollo26.9122020-10-26 16:59:3517.017.21.048.30.00500.9972
2020 TE6Apollo27.4102020-10-18 10:30:5019.016.83.262.90.00270.9975
2020 TS1Aten29.242020-10-12 10:13:049.016.83.637.40.00170.9993
2020 UQ6Apollo22.7862020-10-28 17:30:3517.016.00.416.00.02971.0219
2020 VF4Apollo26.6142020-11-13 16:56:2320.017.02.018.50.00780.9968
2020 VH5Apollo29.242020-11-13 17:33:0421.015.95.47.70.00170.9912
2020 VJ1Apollo26.7132020-11-09 15:23:3020.016.63.134.10.00490.9944
2020 VR1Apollo28.952020-11-09 15:44:3716.017.56.436.10.00260.9925
2020 VZ6Apollo25.0302020-12-02 14:07:0214.014.71.131.00.00490.9900
2020 XHApollo24.6362020-12-05 16:35:3917.016.80.624.20.01651.0004Crowded field
2020 XH1Apollo22.9782020-12-08 12:56:0920.016.70.430.90.03021.0108
2020 XQ2Apollo22.8832020-12-09 15:00:3920.016.60.815.00.03931.0228
2020 XX3Apollo28.562020-12-17 14:09:5218.016.51.038.00.00200.9856
2020 XY4Aten26.9122020-12-20 11:10:5120.017.32.140.30.00590.9883Thin cloud
2020 YJ2Apollo27.4102020-12-21 14:09:0920.016.72.335.70.00390.9869Crowded field
2021 AT5Apollo27.592021-01-13 13:40:0910.016.91.817.90.00500.9884Crowded field
2021 BCAten24.3412021-01-21 10:55:3518.015.91.855.70.00830.9888
2021 CA6Apollo28.562021-02-13 16:03:0422.016.08.166.30.00110.9879
2021 CC7Apollo29.832021-02-12 18:06:5811.017.12.611.50.00210.9894
2021 CGApollo26.1182021-02-06 15:18:4120.017.01.116.70.00980.9957
2021 COApollo25.3262021-02-09 12:12:0521.016.60.27.30.01431.0009
2021 DW1Apollo25.2272021-03-02 11:14:222.016.20.549.20.00700.9957Crowded field
2021 EM4Apollo27.1112021-03-18 16:04:3720.016.81.526.60.00500.9999
2021 EQ3Apollo26.1182021-03-15 11:07:0314.016.61.049.60.00530.9980
2021 ET4Apollo23.9482021-03-16 14:20:1718.017.00.745.10.01841.0078
2021 EX1Apollo24.9322021-03-08 12:53:1120.016.90.522.30.01531.0069
2021 FHApollo26.7132021-03-22 13:13:5120.017.30.321.50.00801.0040Thin cloud
2021 GD5Aten27.1112021-04-08 15:38:3620.018.22.724.30.00981.0104
2021 GQ10Apollo26.6142021-04-14 16:03:0220.015.42.865.70.00201.0040
2021 GT3Apollo26.4162021-04-10 13:03:3220.015.72.111.50.00521.0071
2021 JB6Apollo28.852021-05-13 15:11:1020.016.82.747.30.00171.0118
2021 KN2Apollo28.662021-05-30 16:53:2914.017.12.341.20.00231.0156
2021 KQ2Aten29.932021-05-31 16:27:1020.017.22.939.10.00141.0150
2021 RB1Amor24.1462021-09-06 13:16:1020.016.81.126.50.01991.0258
2021 RX5Apollo23.7542021-09-15 15:25:567.016.60.533.20.01961.0219
2021 TG1Apollo28.272021-10-03 13:22:3220.017.12.539.40.00291.0028
2021 TL14Apollo26.9122021-10-14 14:45:0021.015.72.427.80.00331.0004
2021 TQ3Atira27.1112021-10-06 16:25:1120.017.11.421.30.00621.0055
2021 TQ4Apollo29.932021-10-06 16:54:273.017.33.12.40.00261.0023
2021 TY14Apollo27.2112021-10-15 11:56:3920.017.01.822.20.00561.0023
2021 UF12Apollo29.342021-10-29 14:46:188.016.59.214.00.00190.9951
TMG0042Apollo28.562021-04-10 16:16:1720.0NEO candidate
TMG0049Apollo30.032021-05-30 15:30:0916.0NEO candidate
*

Dynamical class (Dyn. class) and absolute magnitude (H) are from NASA JPL/HORIZONS as of 2022-1-9 (UTC). Observation starting time in UTC (Obs. date) and duration time of observation (T) for each object are listed. V-band apparent magnitude (V), angular rate of change in apparent RA and Dec (Vel.), phase angle (α), distance between NEO and observer (Δ), and distance between Sun and NEO (r) at the observation time are also from NASA JPL/HORIZONS as of 2022-1-9 (UTC).

Diameter (D) is derived from H assuming geometric albedo in V-band of 0.20.

Dyn. class and H of the NEO candidates are derived from orbits determined with the Tomo-e Gozen data using Find_Orb: 〈https://www.projectpluto.com/fo.htm〉.

In this paper, we assume that pV is 0.20, which is a typical value for S-type asteroids, as used in LCDB. The absolute magnitude of 22.5 corresponds to 94 m in diameter. Since a median rotational period of NEOs in LCDB satisfying the quality code U of 3 or 3- and H smaller than 22.5 is about 9 min, we set the nominal duration of observation at 20 min. The mean absolute magnitude of our samples is 26.6, corresponding to 14 m in diameter. As shown in figure 2, the peak of the distribution (H ∼ 26) is smaller than the peak of the targets observed by MANOS (H ∼ 24), hereinafter referred to as the MANOS NEOs.

(Upper panel) Fractional distribution of absolute magnitudes. Tomo-e NEOs and MANOS NEOs are illustrated by solid and dashed lines, respectively. (Lower panel) Absolute magnitude versus geocentric distance of the Tomo-e NEOs (circles) and the MANOS NEOs (crosses) at the observation times. The absolute magnitude and the geocentric distances are referenced from NASA JPL/HORIZONS as of 2021-12-27 (UTC). NEO candidates, TMG0042 and TMG0049, are not included in this figure.
Fig. 2.

(Upper panel) Fractional distribution of absolute magnitudes. Tomo-e NEOs and MANOS NEOs are illustrated by solid and dashed lines, respectively. (Lower panel) Absolute magnitude versus geocentric distance of the Tomo-e NEOs (circles) and the MANOS NEOs (crosses) at the observation times. The absolute magnitude and the geocentric distances are referenced from NASA JPL/HORIZONS as of 2021-12-27 (UTC). NEO candidates, TMG0042 and TMG0049, are not included in this figure.

The Tomo-e NEOs were typically located at a few lunar distances from Earth when observed. A typical angular velocity was about a few arcsec s−1. Most of the Tomo-e NEOs were discovered a few hours or a few days before our observations, except for 2010 WC9, 2011 DW, and 2017 WJ16. TMG0042 and TMG0049 are NEO candidates discovered by Tomo-e Gozen. Due to the limited number of follow-up observations, provisional designations for the two objects were not taken from the Minor Planet Center.

To obtain the light curve of the NEO, we used a single sensor of Tomo-e Gozen with a field of view of |${39{^{\prime }_{.}}7} \times {22{^{\prime }_{.}}4}$| and a pixel scale of |${1{^{\prime \prime}_{.}}189}$|⁠. Sidereal tracking and re-pointing were performed to follow the fast-moving NEOs. All of the Tomo-e NEOs except for 2018 LV3 were observed at 2 fps. The light curve of 2018 LV3 was obtained at 0.2 fps as an experimental observation.

2.2 Data reduction

2.2.1 Photometry

Observations are composed of a series of video data which were typically 1 min in length. The video data were compiled into cube FITS files. After bias and dark subtraction and flat-field correction, standard circle aperture photometry was performed on a target and reference stars in each frame using the SExtractor-based python package sep (Bertin & Arnouts 1996; K. Barbary et al. 20154). Since the elongations of the NEOs were negligible, we applied the standard aperture photometry method. The aperture radius was set to two to three times larger than the full width at half maximum (FWHM) of the point spread function (PSF) of reference stars, which was typically 3″ to 5″. We determined the FWHM of the stellar PSF in the first frame of the cube, and then conducted the photometry of the objects in each frame. Sometimes the target was too faint to be detected, possibly because of the brightness variation of the target. In such cases, we set the aperture at the expected positions interpolated from the positions in adjacent frames and performed forced photometry.

We used the G-band magnitude from the Gaia DR2 catalog as brightness references since the spectral response of Tomo-e Gozen (350 to 950 nm; Kojima et al. 2018) is similar to that of the G-band of Gaia (330 to 1050 nm; Gaia Collaboration 2018). The difference in the spectral responses may affect the mean apparent magnitudes of the NEOs, but the rotational period is not affected by the spectral response and the effect on the amplitudes is negligible. The discussion in this paper is not affected.

The G-band magnitude of a NEO, mG, on each frame was derived as follows:
(2)
where F is the total flux in the aperture and Z is the magnitude zero-point of the frame. Stars with G-band magnitudes 10 < mG < 15 and broad-band colors −1 < GBPGBP < 1, typically 20–30, were used to calculate the magnitude zero points, and the median value of the zero points was used as Z. The uncertainty of Z was estimated from the median absolute deviation of the zero points. The photometric error of the NEO consists of the background noise, the Poisson noise, and the uncertainty of Z.

The observed G-band magnitudes were converted to reduced magnitudes with the distance between the Sun and NEO (r) and NEO and observer (Δ) at the time of observations. The phase angle correction and the light-travel time correction were done to obtain the corrected light curves.

2.2.2 Periodic analysis

We used the Lomb–Scargle technique to estimate rotational periods from non-evenly sampled data (Lomb 1976; Scargle 1982; VanderPlas 2018). Fitting models are given by the following form:
(3)
where f is a frequency, c0 denotes the average brightness, n is the number of harmonics, and Si and Ci are the Fourier coefficients of the ith harmonics. The normalized residual χ2 was calculated as
(4)
where nobs is the number of observation data, tj is the observation time of the jth sample, and yobs, j and yerr, j are the jth measured brightness and its uncertainty, respectively. We calculated the Lomb–Scargle periodogram PLS as
(5)
where |$\chi _0^2$| is the χ2(f) for a constant fitting model where Si and Ci are set to zero for all i.
The significance of a peak in a periodogram is evaluated by calculating a confidence level against the null hypothesis. Assuming that the data consists of pure Gaussian noise, 2PLS follows a χ2 distribution with two degrees of freedom when n = 1. Thus,
(6)
expresses a cumulative probability that PLS is less than z at each frequency. We assumed that the frequencies are independent of each other and defined an effective number of frequencies as
(7)
where fmax is the maximum frequency to be considered. A false alarm probability, FAP(z), is calculated as follows:
(8)
We calculated a |$99.9\%$| confidence level in each periodogram. We derived a candidate of the rotational period from the highest peak of PLS larger than the |$99.9\%$| confidence level.
For optimal determination of the number of harmonics n, we used the Akaike Information Criterion (AIC; Akaike 1974). AIC indicates the trade-off between the goodness of fit and the simplicity of the model. AIC is calculated as
(9)
where L is the likelihood of the parameters. We adopted n of each NEO for which AIC value is the minimum.

The uncertainty of the rotational period and the light-curve amplitude were estimated using the Monte Carlo method. We created 3000 light curves for each NEO by randomly resampling the data assuming each observed data follows a normal distribution the standard deviation of which is a photometric error. We performed the same analyses above for 3000 light curves and obtained 3000 sets of Fourier coefficients in equation (3). We calculated the 3000 periods and the 3000 amplitude with the corresponding peak frequencies for each light curve. As an example, the analysis result of 2021 CG is shown in figure 3. We adopted the standard deviations as the uncertainties of the period and the amplitude. If the estimated standard deviation was larger than |$5\%$| of the rotational period, we judged that the derived rotational period was suspicious and the correct rotational period was not derived. We used the Fourier coefficients of which the rotational period and the light curve amplitude are the closest to the average values to plot a typical model curve.

Scatter plot of the rotational periods and the light curve amplitudes of 3000 model curves of 2021 CG. Histograms at the top and to the side present the marginal distributions of the periods and the amplitudes, respectively. The derived period and amplitude are represented by a square symbol with a cross that indicates the standard deviations of the period and the amplitude.
Fig. 3.

Scatter plot of the rotational periods and the light curve amplitudes of 3000 model curves of 2021 CG. Histograms at the top and to the side present the marginal distributions of the periods and the amplitudes, respectively. The derived period and amplitude are represented by a square symbol with a cross that indicates the standard deviations of the period and the amplitude.

There are several candidates of non-principal axis rotators (i.e., tumbler) in the Tomo-e NEOs. The tumbler is in a excited state and its light curve is complicated (e.g., Paolicchi et al. 2002; Pravec et al. 2005). Therefore, the periodograms of the tumblers show additional peaks which are not aliases of the highest peak. We defined such objects with multiple peaks as tumbler candidates in this paper.

3 Results

We successfully derived the rotational periods of 32 NEOs. Results of the analysis are summarized in table 2. The rotational periods of 11 out of the 32 are reported in previous studies: 2019 BE5 (Warner et al. 2009), 2020 TD8, 2020 UQ6, 2020 VZ6, 2020 XX3 (Birtwhistle 2021a), 2021 EX1, 2021 FH (Birtwhistle 2021b), 2021 KN2, 2021 JB6, 2021 GQ10 (Birtwhistle 2021c), and 2021 DW1 (Kwiatkowski et al. 2021). All our results are consistent with the reported values. The periodogram of 2021 FH has a prominent peak but its significance level is lower than |$99.9\%$|⁠. We considered that the peak of 2021 FH is reliable since the peak frequency corresponds to the rotational period (63.4 s) reported by Birtwhistle (2021b).

Table 2.

Summary of observational results.*

ObjectHDNobsnPΔma/bNote
(mag)(m)(s)(mag)
2010 WC923.559670Known tumbler
2011 DW22.9792099> 1320
2017 WJ1624.537135Tumbler
2114Tumbler
2018 LV326.5157003415.9 ± 0.40.46 ± 0.03≥ 1.245  s exposure
2018 UD326.21739771229.720 ± 0.0030.55 ± 0.02≥ 1.22
2019 BE525.1281125411.97902 ± 0.000090.80 ± 0.04≥ 1.40
2020 EO25.9201483Tumbler
2020 FA227.5949306150.67 ± 0.020.26 ± 0.01≥ 1.15
2020 FL226.11815579325.1 ± 0.80.102 ± 0.005≥ 1.07
2020 GY126.61414746303 ± 30.17 ±  0.02≥ 1.10
2020 HK324.2431476> 780
2020 HS729.14136512.9945 ± 0.00020.069 ± 0.006≥ 1.04
89622.9938 ± 0.00020.075 ± 0.006≥ 1.04
2020 HT726.9121411645.80 ± 0.010.38 ± 0.02≥ 1.17
2020 HU326.019666> 360
2020 PW228.851198887.6 ± 0.60.54 ±  0.06≥ 1.33
2020 PY226.5151815619.835 ± 0.0020.28 ± 0.01≥ 1.21
2020 QW25.3261102> 1200
2020 TD826.912434529.53 ± 0.011.19 ± 0.04≥ 1.56
2020 TE627.4101537Tumbler
2020 TS129.24793> 540
2020 UQ622.786173013162.82 ± 0.030.819 ± 0.009≥ 1.66
2020 VF426.6141808> 1200
2020 VH529.2420987157.6 ± 0.40.15 ± 0.01≥ 1.12
2020 VJ126.71393813241 ± 10.64 ±  0.05≥ 1.34
2020 VR128.95677> 1200
2020 VZ625.030162210353.4 ± 0.21.06 ± 0.02≥ 1.66
2020 XH24.636208> 1020
2020 XH122.9781912> 1200
2020 XQ222.883244> 1200
2020 XX328.56166413136.22 ± 0.050.98 ± 0.02≥ 1.52
2020 XY426.91220203324 ± 60.15 ±  0.01≥ 1.06
2020 YJ227.410182> 1200
2021 AT527.59458> 600
2021 BC24.3411382> 1200
2021 CA628.562219614.3159 ± 0.00040.694 ± 0.008≥ 1.24
2021 CC729.831109413.510 ± 0.0040.25 ± 0.02≥ 1.19
2021 CG26.1181857915.296 ± 0.0020.27 ± 0.02≥ 1.18
2021 CO25.3261603Known tumbler
2021 DW125.227146423.8 ± 0.20.68 ±  0.08≥ 1.29
2021 EM427.1111438899.5 ± 0.40.26 ± 0.03≥ 1.14
2021 EQ326.118137611119.41 ± 0.020.71 ± 0.02≥ 1.30
2021 ET423.9481703487.8 ± 0.20.21 ± 0.02≥ 1.09
2021 EX124.93222274410 ± 10.222 ± 0.009≥ 1.13
2021 FH26.7131632363.5 ± 0.60.16 ± 0.02≥ 1.09
2021 GD527.1112240> 1200
2021 GQ1026.6141167319.308 ± 0.0030.192 ± 0.007≥ 1.06
2021 GT326.416201310155.1 ± 0.20.149 ± 0.009≥ 1.11
2021 JB628.852212265.64 ± 0.020.55 ± 0.01≥ 1.23
2021 KN228.661244Known tumbler
2021 KQ229.931829Tumbler
2021 RB124.1461931> 1200
2021 RX523.754528> 420
2021 TG128.27780Tumbler
2021 TL1426.9121626Tumbler
2021 TQ327.1111897> 1200
2021 TQ429.93424Tumbler
2021 TY1427.2112051415.292 ± 0.0020.61 ± 0.02≥ 1.40
2021 UF1229.34423114.860 ± 0.0040.51 ± 0.02≥ 1.39
TMG004228.56193720314.4 ± 0.31.00 ± 0.04≥ 2.51
TMG004930.031538> 1080
ObjectHDNobsnPΔma/bNote
(mag)(m)(s)(mag)
2010 WC923.559670Known tumbler
2011 DW22.9792099> 1320
2017 WJ1624.537135Tumbler
2114Tumbler
2018 LV326.5157003415.9 ± 0.40.46 ± 0.03≥ 1.245  s exposure
2018 UD326.21739771229.720 ± 0.0030.55 ± 0.02≥ 1.22
2019 BE525.1281125411.97902 ± 0.000090.80 ± 0.04≥ 1.40
2020 EO25.9201483Tumbler
2020 FA227.5949306150.67 ± 0.020.26 ± 0.01≥ 1.15
2020 FL226.11815579325.1 ± 0.80.102 ± 0.005≥ 1.07
2020 GY126.61414746303 ± 30.17 ±  0.02≥ 1.10
2020 HK324.2431476> 780
2020 HS729.14136512.9945 ± 0.00020.069 ± 0.006≥ 1.04
89622.9938 ± 0.00020.075 ± 0.006≥ 1.04
2020 HT726.9121411645.80 ± 0.010.38 ± 0.02≥ 1.17
2020 HU326.019666> 360
2020 PW228.851198887.6 ± 0.60.54 ±  0.06≥ 1.33
2020 PY226.5151815619.835 ± 0.0020.28 ± 0.01≥ 1.21
2020 QW25.3261102> 1200
2020 TD826.912434529.53 ± 0.011.19 ± 0.04≥ 1.56
2020 TE627.4101537Tumbler
2020 TS129.24793> 540
2020 UQ622.786173013162.82 ± 0.030.819 ± 0.009≥ 1.66
2020 VF426.6141808> 1200
2020 VH529.2420987157.6 ± 0.40.15 ± 0.01≥ 1.12
2020 VJ126.71393813241 ± 10.64 ±  0.05≥ 1.34
2020 VR128.95677> 1200
2020 VZ625.030162210353.4 ± 0.21.06 ± 0.02≥ 1.66
2020 XH24.636208> 1020
2020 XH122.9781912> 1200
2020 XQ222.883244> 1200
2020 XX328.56166413136.22 ± 0.050.98 ± 0.02≥ 1.52
2020 XY426.91220203324 ± 60.15 ±  0.01≥ 1.06
2020 YJ227.410182> 1200
2021 AT527.59458> 600
2021 BC24.3411382> 1200
2021 CA628.562219614.3159 ± 0.00040.694 ± 0.008≥ 1.24
2021 CC729.831109413.510 ± 0.0040.25 ± 0.02≥ 1.19
2021 CG26.1181857915.296 ± 0.0020.27 ± 0.02≥ 1.18
2021 CO25.3261603Known tumbler
2021 DW125.227146423.8 ± 0.20.68 ±  0.08≥ 1.29
2021 EM427.1111438899.5 ± 0.40.26 ± 0.03≥ 1.14
2021 EQ326.118137611119.41 ± 0.020.71 ± 0.02≥ 1.30
2021 ET423.9481703487.8 ± 0.20.21 ± 0.02≥ 1.09
2021 EX124.93222274410 ± 10.222 ± 0.009≥ 1.13
2021 FH26.7131632363.5 ± 0.60.16 ± 0.02≥ 1.09
2021 GD527.1112240> 1200
2021 GQ1026.6141167319.308 ± 0.0030.192 ± 0.007≥ 1.06
2021 GT326.416201310155.1 ± 0.20.149 ± 0.009≥ 1.11
2021 JB628.852212265.64 ± 0.020.55 ± 0.01≥ 1.23
2021 KN228.661244Known tumbler
2021 KQ229.931829Tumbler
2021 RB124.1461931> 1200
2021 RX523.754528> 420
2021 TG128.27780Tumbler
2021 TL1426.9121626Tumbler
2021 TQ327.1111897> 1200
2021 TQ429.93424Tumbler
2021 TY1427.2112051415.292 ± 0.0020.61 ± 0.02≥ 1.40
2021 UF1229.34423114.860 ± 0.0040.51 ± 0.02≥ 1.39
TMG004228.56193720314.4 ± 0.31.00 ± 0.04≥ 2.51
TMG004930.031538> 1080
*

Nobs is the number of frames. n is the number of harmonics of the model curve. P is the rotational period. Δm is the light-curve amplitude. a/b is the axial ratio of the asteroid derived from Δm.

Table 2.

Summary of observational results.*

ObjectHDNobsnPΔma/bNote
(mag)(m)(s)(mag)
2010 WC923.559670Known tumbler
2011 DW22.9792099> 1320
2017 WJ1624.537135Tumbler
2114Tumbler
2018 LV326.5157003415.9 ± 0.40.46 ± 0.03≥ 1.245  s exposure
2018 UD326.21739771229.720 ± 0.0030.55 ± 0.02≥ 1.22
2019 BE525.1281125411.97902 ± 0.000090.80 ± 0.04≥ 1.40
2020 EO25.9201483Tumbler
2020 FA227.5949306150.67 ± 0.020.26 ± 0.01≥ 1.15
2020 FL226.11815579325.1 ± 0.80.102 ± 0.005≥ 1.07
2020 GY126.61414746303 ± 30.17 ±  0.02≥ 1.10
2020 HK324.2431476> 780
2020 HS729.14136512.9945 ± 0.00020.069 ± 0.006≥ 1.04
89622.9938 ± 0.00020.075 ± 0.006≥ 1.04
2020 HT726.9121411645.80 ± 0.010.38 ± 0.02≥ 1.17
2020 HU326.019666> 360
2020 PW228.851198887.6 ± 0.60.54 ±  0.06≥ 1.33
2020 PY226.5151815619.835 ± 0.0020.28 ± 0.01≥ 1.21
2020 QW25.3261102> 1200
2020 TD826.912434529.53 ± 0.011.19 ± 0.04≥ 1.56
2020 TE627.4101537Tumbler
2020 TS129.24793> 540
2020 UQ622.786173013162.82 ± 0.030.819 ± 0.009≥ 1.66
2020 VF426.6141808> 1200
2020 VH529.2420987157.6 ± 0.40.15 ± 0.01≥ 1.12
2020 VJ126.71393813241 ± 10.64 ±  0.05≥ 1.34
2020 VR128.95677> 1200
2020 VZ625.030162210353.4 ± 0.21.06 ± 0.02≥ 1.66
2020 XH24.636208> 1020
2020 XH122.9781912> 1200
2020 XQ222.883244> 1200
2020 XX328.56166413136.22 ± 0.050.98 ± 0.02≥ 1.52
2020 XY426.91220203324 ± 60.15 ±  0.01≥ 1.06
2020 YJ227.410182> 1200
2021 AT527.59458> 600
2021 BC24.3411382> 1200
2021 CA628.562219614.3159 ± 0.00040.694 ± 0.008≥ 1.24
2021 CC729.831109413.510 ± 0.0040.25 ± 0.02≥ 1.19
2021 CG26.1181857915.296 ± 0.0020.27 ± 0.02≥ 1.18
2021 CO25.3261603Known tumbler
2021 DW125.227146423.8 ± 0.20.68 ±  0.08≥ 1.29
2021 EM427.1111438899.5 ± 0.40.26 ± 0.03≥ 1.14
2021 EQ326.118137611119.41 ± 0.020.71 ± 0.02≥ 1.30
2021 ET423.9481703487.8 ± 0.20.21 ± 0.02≥ 1.09
2021 EX124.93222274410 ± 10.222 ± 0.009≥ 1.13
2021 FH26.7131632363.5 ± 0.60.16 ± 0.02≥ 1.09
2021 GD527.1112240> 1200
2021 GQ1026.6141167319.308 ± 0.0030.192 ± 0.007≥ 1.06
2021 GT326.416201310155.1 ± 0.20.149 ± 0.009≥ 1.11
2021 JB628.852212265.64 ± 0.020.55 ± 0.01≥ 1.23
2021 KN228.661244Known tumbler
2021 KQ229.931829Tumbler
2021 RB124.1461931> 1200
2021 RX523.754528> 420
2021 TG128.27780Tumbler
2021 TL1426.9121626Tumbler
2021 TQ327.1111897> 1200
2021 TQ429.93424Tumbler
2021 TY1427.2112051415.292 ± 0.0020.61 ± 0.02≥ 1.40
2021 UF1229.34423114.860 ± 0.0040.51 ± 0.02≥ 1.39
TMG004228.56193720314.4 ± 0.31.00 ± 0.04≥ 2.51
TMG004930.031538> 1080
ObjectHDNobsnPΔma/bNote
(mag)(m)(s)(mag)
2010 WC923.559670Known tumbler
2011 DW22.9792099> 1320
2017 WJ1624.537135Tumbler
2114Tumbler
2018 LV326.5157003415.9 ± 0.40.46 ± 0.03≥ 1.245  s exposure
2018 UD326.21739771229.720 ± 0.0030.55 ± 0.02≥ 1.22
2019 BE525.1281125411.97902 ± 0.000090.80 ± 0.04≥ 1.40
2020 EO25.9201483Tumbler
2020 FA227.5949306150.67 ± 0.020.26 ± 0.01≥ 1.15
2020 FL226.11815579325.1 ± 0.80.102 ± 0.005≥ 1.07
2020 GY126.61414746303 ± 30.17 ±  0.02≥ 1.10
2020 HK324.2431476> 780
2020 HS729.14136512.9945 ± 0.00020.069 ± 0.006≥ 1.04
89622.9938 ± 0.00020.075 ± 0.006≥ 1.04
2020 HT726.9121411645.80 ± 0.010.38 ± 0.02≥ 1.17
2020 HU326.019666> 360
2020 PW228.851198887.6 ± 0.60.54 ±  0.06≥ 1.33
2020 PY226.5151815619.835 ± 0.0020.28 ± 0.01≥ 1.21
2020 QW25.3261102> 1200
2020 TD826.912434529.53 ± 0.011.19 ± 0.04≥ 1.56
2020 TE627.4101537Tumbler
2020 TS129.24793> 540
2020 UQ622.786173013162.82 ± 0.030.819 ± 0.009≥ 1.66
2020 VF426.6141808> 1200
2020 VH529.2420987157.6 ± 0.40.15 ± 0.01≥ 1.12
2020 VJ126.71393813241 ± 10.64 ±  0.05≥ 1.34
2020 VR128.95677> 1200
2020 VZ625.030162210353.4 ± 0.21.06 ± 0.02≥ 1.66
2020 XH24.636208> 1020
2020 XH122.9781912> 1200
2020 XQ222.883244> 1200
2020 XX328.56166413136.22 ± 0.050.98 ± 0.02≥ 1.52
2020 XY426.91220203324 ± 60.15 ±  0.01≥ 1.06
2020 YJ227.410182> 1200
2021 AT527.59458> 600
2021 BC24.3411382> 1200
2021 CA628.562219614.3159 ± 0.00040.694 ± 0.008≥ 1.24
2021 CC729.831109413.510 ± 0.0040.25 ± 0.02≥ 1.19
2021 CG26.1181857915.296 ± 0.0020.27 ± 0.02≥ 1.18
2021 CO25.3261603Known tumbler
2021 DW125.227146423.8 ± 0.20.68 ±  0.08≥ 1.29
2021 EM427.1111438899.5 ± 0.40.26 ± 0.03≥ 1.14
2021 EQ326.118137611119.41 ± 0.020.71 ± 0.02≥ 1.30
2021 ET423.9481703487.8 ± 0.20.21 ± 0.02≥ 1.09
2021 EX124.93222274410 ± 10.222 ± 0.009≥ 1.13
2021 FH26.7131632363.5 ± 0.60.16 ± 0.02≥ 1.09
2021 GD527.1112240> 1200
2021 GQ1026.6141167319.308 ± 0.0030.192 ± 0.007≥ 1.06
2021 GT326.416201310155.1 ± 0.20.149 ± 0.009≥ 1.11
2021 JB628.852212265.64 ± 0.020.55 ± 0.01≥ 1.23
2021 KN228.661244Known tumbler
2021 KQ229.931829Tumbler
2021 RB124.1461931> 1200
2021 RX523.754528> 420
2021 TG128.27780Tumbler
2021 TL1426.9121626Tumbler
2021 TQ327.1111897> 1200
2021 TQ429.93424Tumbler
2021 TY1427.2112051415.292 ± 0.0020.61 ± 0.02≥ 1.40
2021 UF1229.34423114.860 ± 0.0040.51 ± 0.02≥ 1.39
TMG004228.56193720314.4 ± 0.31.00 ± 0.04≥ 2.51
TMG004930.031538> 1080
*

Nobs is the number of frames. n is the number of harmonics of the model curve. P is the rotational period. Δm is the light-curve amplitude. a/b is the axial ratio of the asteroid derived from Δm.

The rotational periods of 18 objects were not derived due to small amplitudes. These objects may have axisymmetric shapes, rotational periods longer than the duration of observation, rotational periods shorter than the exposure time, or rotational axes parallel to the line of sight. When a light curve shows a clear brightness variation but whole cycles of rotation were not obtained, we adopted the duration times of the observations as lower limits of rotational periods.

We found 10 tumbler candidates: 2010 WC9, 2017 WJ16, 2020 TE6, 2021 CO, 2020 EO, 2021 KN2, 2021 KQ2, 2021 TG1, 2021 TL14, and 2021 TQ4. Physical modeling of these candidates will be presented elsewhere.

3.1 Light curves and periodograms

As an example, we presented the light curve and periodogram of 2021 CG in figures 4 and 5, respectively. The rotational period and the light curve amplitude of 2021 CG were estimated to be 15.296 ± 0.002 s and 0.27 ± 0.02 mag, respectively, using the Monte Carlo method as shown in figure 3. The light curve folded by the rotational period (hereinafter referred to as the phased light curve) is shown in figure 6. Thanks to the video observations at 2 fps, we can estimate such a short period of rotation with high reliability. (The light curves, periodograms of 60 NEOs, and phased light curves of NEOs whose rotational periods were estimated are presented in figures 1416 in the Appendix.)

Light curve of 2021 CG. The first 100 s part of the whole 20 min light curve is plotted. Bars indicate the 1σ uncertainties (see text for details).
Fig. 4.

Light curve of 2021 CG. The first 100 s part of the whole 20 min light curve is plotted. Bars indicate the 1σ uncertainties (see text for details).

Lomb–Scargle periodogram of 2021 CG. The number of harmonics is unity. Solid, dashed, and dot–dashed horizontal lines show 90.0, 99.0, and $99.9\%$ confidence levels, respectively.
Fig. 5.

Lomb–Scargle periodogram of 2021 CG. The number of harmonics is unity. Solid, dashed, and dot–dashed horizontal lines show 90.0, 99.0, and |$99.9\%$| confidence levels, respectively.

Phased light curve of 2021 CG. A model curve with a period of 15.296 s and a light curve amplitude of 0.27 mag is shown by a dashed line. Photometric errors are the same as in figure 4.
Fig. 6.

Phased light curve of 2021 CG. A model curve with a period of 15.296 s and a light curve amplitude of 0.27 mag is shown by a dashed line. Photometric errors are the same as in figure 4.

D–P relations of the Tomo-e NEOs (open circles) and the NEOs in LCDB (filled circles). The range of detectable rotational period of our targets (D ≤ 100 m), 1.5 s to 10 min, in typical observations at 2 fps for 20 min with Tomo-e Gozen is shown as a gray shaded area.
Fig. 7.

D–P relations of the Tomo-e NEOs (open circles) and the NEOs in LCDB (filled circles). The range of detectable rotational period of our targets (D ≤ 100 m), 1.5 s to 10 min, in typical observations at 2 fps for 20 min with Tomo-e Gozen is shown as a gray shaded area.

Cumulative histograms of rotational periods of the Tomo-e Gozen NEOs (solid line) and the NEOs in LCDB (dashed line) with absolute magnitudes larger than 22.5 and rotational periods shorter than 420 s.
Fig. 8.

Cumulative histograms of rotational periods of the Tomo-e Gozen NEOs (solid line) and the NEOs in LCDB (dashed line) with absolute magnitudes larger than 22.5 and rotational periods shorter than 420 s.

Absolute magnitude versus lower limits of axial ratios of the Tomo-e (open circles) and the MANOS NEOs (crosses) with rotational periods shorter than 600 s. The mean value in each range is presented by a diamond and a triangle for the Tomo-e NEOs and the MANOS NEOs, respectively. Vertical bars indicate standard deviations.
Fig. 9.

Absolute magnitude versus lower limits of axial ratios of the Tomo-e (open circles) and the MANOS NEOs (crosses) with rotational periods shorter than 600 s. The mean value in each range is presented by a diamond and a triangle for the Tomo-e NEOs and the MANOS NEOs, respectively. Vertical bars indicate standard deviations.

Rotational periods versus lower limits of axial ratios of the Tomo-e (open circles) and the MANOS NEOs (crosses) with rotational periods shorter than 600 s. The mean value in each range is presented by a diamond and a triangle for the Tomo-e NEOs and the MANOS NEOs, respectively. Vertical bars indicate standard deviations.
Fig. 10.

Rotational periods versus lower limits of axial ratios of the Tomo-e (open circles) and the MANOS NEOs (crosses) with rotational periods shorter than 600 s. The mean value in each range is presented by a diamond and a triangle for the Tomo-e NEOs and the MANOS NEOs, respectively. Vertical bars indicate standard deviations.

Diameter versus lower limits of axial ratios of tiny NEOs, fast-rotating asteroids (FRAs), and apparent axis ratios of boulders on Itokawa and Ryugu. Mean values of tiny NEOs and FRAs are presented as solid and dashed lines, respectively. Typical values of boulders on Itokawa and Ryugu are presented as dotted and dash–dotted lines, respectively. Fractions of each range of axial ratio for tiny NEOs and FRAs are shown as histograms in the right-hand panel. NEOs with axial ratios larger than 2.0 are not shown in the figures but are used in calculations.
Fig. 11.

Diameter versus lower limits of axial ratios of tiny NEOs, fast-rotating asteroids (FRAs), and apparent axis ratios of boulders on Itokawa and Ryugu. Mean values of tiny NEOs and FRAs are presented as solid and dashed lines, respectively. Typical values of boulders on Itokawa and Ryugu are presented as dotted and dash–dotted lines, respectively. Fractions of each range of axial ratio for tiny NEOs and FRAs are shown as histograms in the right-hand panel. NEOs with axial ratios larger than 2.0 are not shown in the figures but are used in calculations.

D–P relations of NEOs with the isochrones (solid lines). The Tomo-e NEOs and the NEOs in LCDB are presented with open and filled circles, respectively. (a) D–P relation with the collisional initial line (dashed line). (b) D–P relation with lines of critical rotational periods when asteroids have tensile strength of a typical meteorite (dashed line) and weak material (dot–dashed line). (c) D–P relation with lower limits by angular momentum transfers due to meteoroid impacts with δL/L = 0.01 (dashed line), 0.08 (dot–dashed line), and 0.085 (dotted line). (d) D–P relation with lower limits by cratering due to meteoroid impacts with m0 of 2 × 10−6 kg (dashed-line), 2 × 10−4 kg (dot–dashed line), and 2 × 10−2 kg (dotted line). See text for details.
Fig. 12.

D–P relations of NEOs with the isochrones (solid lines). The Tomo-e NEOs and the NEOs in LCDB are presented with open and filled circles, respectively. (a) D–P relation with the collisional initial line (dashed line). (b) D–P relation with lines of critical rotational periods when asteroids have tensile strength of a typical meteorite (dashed line) and weak material (dot–dashed line). (c) D–P relation with lower limits by angular momentum transfers due to meteoroid impacts with δL/L = 0.01 (dashed line), 0.08 (dot–dashed line), and 0.085 (dotted line). (d) D–P relation with lower limits by cratering due to meteoroid impacts with m0 of 2 × 10−6 kg (dashed-line), 2 × 10−4 kg (dot–dashed line), and 2 × 10−2 kg (dotted line). See text for details.

D–P relations of NEOs with isochrones considering the TYORP effect. The Tomo-e NEOs and the NEOs in LCDB are represented by open and filled circles, respectively. (a) Case with θmax of 5. (b) Case with θmax of 30. Isochrones that are 10 Myr old with γ of 0.1 and 0.5 are shown by solid and dashed lines, respectively. Arrows indicate positions where θ reaches θmax.
Fig. 13.

D–P relations of NEOs with isochrones considering the TYORP effect. The Tomo-e NEOs and the NEOs in LCDB are represented by open and filled circles, respectively. (a) Case with θmax of 5. (b) Case with θmax of 30. Isochrones that are 10 Myr old with γ of 0.1 and 0.5 are shown by solid and dashed lines, respectively. Arrows indicate positions where θ reaches θmax.

Fig. 14.

From left to right: full light curves from the exposure starting time, partial light curves, Lomb–Scargle periodograms with n of 1, and phased light curves of the NEOs whose rotational periods are derived with high reliability. Solid, dashed, and dot–dashed horizontal lines in the periodograms show |$90.0\%$|⁠, |$99.0\%$|⁠, and |$99.9\%$| confidence levels, respectively. Confidence lines of some NEOs with strong peaks are hard to see due to scale effects. Dashed lines in the phased light curves show the model curves. Twice the rotational periods are adopted as time ranges of the partial light curves.

Fig. 15.

Full light curves and Lomb–Scargle periodograms of the NEOs whose rotational periods are not derived. The same as the two left-hand columns in figure 14.

Full light curves and Lomb–Scargle periodograms of the tumbler candidates. The same as the two left-hand columns in figure 14.
Fig. 16.

Full light curves and Lomb–Scargle periodograms of the tumbler candidates. The same as the two left-hand columns in figure 14.

3.2 D–P relation

The D–P relation of the Tomo-e NEOs and the NEOs in LCDB is shown in figure 7. The Tomo-e NEOs are distributed in a range of 3 to 100 m in diameter and 3 to 420 s in rotational period. We found 13 NEOs with rotational periods less than 60 s.

We create cumulative histograms of rotational periods of the Tomo-e NEOs and the NEOs in LCDB (figure 8). The D–P relation of the Tomo-e NEOs looks different from that of the NEOs in LCDB. We performed the Kolmogorov–Smirnov (KS) test to check the null hypothesis that the two D–P relations are the same. We chose the NEOs satisfying the criteria that the absolute magnitude is larger than 22.5 and the rotational period is shorter than 420 s corresponding to the longest rotational period of the Tomo-e NEOs. The NEOs which had quality codes 3 or 3- are used as for the NEOs in LCDB. The deduced KS statistics and the p-value are 0.330 and 0.013, respectively. This tentatively implies that rotational periods of some fast rotators could not be estimated due to long exposure times and other factors in the previous studies.

3.3 Axial ratios

We defined the light curve amplitude Δm by the difference between maximum and minimum values of the model curve. We assumed the asteroid is a triaxial ellipsoid with axial lengths of a, b, and c (a > b > c) and the aspect angle of 90°. A lower limit of axial ratio a/b is estimated as follows:
(10)
where Δm(α) is the light curve amplitude at a phase angle of α and s is a slope depending on the taxonomic type of the asteroid (Bowell et al. 1989). We assumed that s is 0.030, a typical value of S-type asteroids (Zappala et al. 1990).

The relation between the absolute magnitudes H and the lower limits of axial ratios a/b of the Tomo-e NEOs and the MANOS NEOs with rotational periods shorter than 600 s are shown in figure 9. The relation between the rotational period P and a/b of the Tomo-e NEOs and the MANOS NEOs with P ≤ 600 s are shown in figure 10. The mean of a/b for each range of H and P is also presented. The range is determined based on the Sturges’ rule. No strong correlation is seen in either figure 9 or 10. The present results are consistent with those of Hatch and Wiegert (2015) and Thirouin et al. (2016).

The difference of mean axial ratios between the Tomo-e NEOs (∼1.29) and the MANOS NEOs (∼1.27) is about 0.02. We performed a bootstrap test to check the null hypothesis that the mean axial ratios of the two samples are the same. We generated 10000 differences of the mean axial ratios by resampling the Tomo-e and MANOS NEOs. The |$95\%$| confidence interval is from −0.08 to 0.14. Thus, the null hypothesis is not rejected at the |$5\%$| significance level.

Figure 11 shows measured a/b of various sources: the average of the sum of the Tomo-e NEOs and the MANOS NEOs, the average of fast-rotating asteroids (FRAs) with diameters less than 200 m and a rotational period less than 1 hr (Michikami et al. 2010), and the averages of boulders on the surfaces of asteroids Itokawa (Michikami et al. 2010) and Ryugu (Michikami et al. 2019).

Michikami et al. (2010) mention that the lower limits of a/b of FRAs and the a/b of boulders are similar to those of laboratory experiments (∼1.4), although the aspect angles of asteroids are unknown. The lower limits of a/b of asteroids are lower in the case of recent observational results such as Tomo-e Gozen (∼1.29) and MANOS (∼1.27). It is important not only to increase the number of light curve observations, but also to determine pole directions to discuss the relation with fragments of laboratory experiments and boulders (e.g., Kwiatkowski et al. 2021).

4 Discussion

4.1 Detectable rotational period

Sparse sampling and finite exposure time may lead to underestimating the light curve amplitude and misidentifying periodicity (Pravec & Harris 2000; Thirouin et al. 2018; Birtwhistle 2021c). We examine detection limits in rotational periods (Pdet) in our observations to verify the deficiency of asteroids rotating faster than 10 s. We simulate light curves if an asteroid was rotating faster than it is, and then the light curves are analyzed in the same manner. We selected eight NEOs with rotational periods that are short (P ≤ 60 s), and the durations of the observations are typical (10 ≤ T ≤ 30 min). We excluded 2020 HS7 from this examination since its exposure time is not sufficiently shorter than the rotational period and the observed light curve could be underestimated (Birtwhistle 2021c). The model light curves of the eight NEOs are used as templates. The rotational period of a hypothetical asteroid Ppseudo is set to Ppseudo = P/2, P/3, P/4, ..., where P is the original rotational period in section 3. Then, the hypothetical asteroid is virtually observed to generate a pseudo light curve. The number of measurements (Nobs) and the timestamps are the same as the actual observation. The pseudo light curve is perturbed to match the noise level with the original observation. The criterion of the periodicity identification is the same as in sub-subsection 2.2.2.

The results of the periodic analysis are summarized in table 3. The detectable rotational periods are less than 2 s for all the eight asteroids. Although our observations are unevenly sampled because of intervals between frames, large fractions of the data are evenly sampled at 2 fps. The periodograms of the pseudo light curves can be affected by aliases when the frequency gets closer to the Nyquist limit fNy = 2/2 = 1 Hz. However, the peaks by the aliases become weaker than the genuine peaks due to the uneven sampling. Thus, it is natural that we detect shorter rotational periods than the Nyquist limit (P = 2 s assuming typical double-peak light curves). We conservatively set the detectable rotational period to 1.5 s in our systematic 20 min video observations at 2 fps. Therefore, it is inevitable that there is only one fast rotator whose rotational period is shorter than 10 s from our 60 NEOs.

Table 3.

Periodic analysis results of pseudo light curves.

ObjectNdetPdet* (s)
pseudo 2020 HT714111.3086 ± 0.0001
pseudo 2020 PY218151.32235 ± 0.00002
pseudo 2020 TD84341.2302 ± 0.0001
pseudo 2021 CA622191.301436 ± 0.000007
pseudo 2021 CC711091.501 ± 0.001
pseudo 2021 CG18571.3906 ± 0.0002
pseudo 2021 GQ1011671.20683 ± 0.00004
pseudo 2021 TY1420511.27431 ± 0.00006
ObjectNdetPdet* (s)
pseudo 2020 HT714111.3086 ± 0.0001
pseudo 2020 PY218151.32235 ± 0.00002
pseudo 2020 TD84341.2302 ± 0.0001
pseudo 2021 CA622191.301436 ± 0.000007
pseudo 2021 CC711091.501 ± 0.001
pseudo 2021 CG18571.3906 ± 0.0002
pseudo 2021 GQ1011671.20683 ± 0.00004
pseudo 2021 TY1420511.27431 ± 0.00006
*

Pdet is the detectable rotational period of the object with the same observational conditions in this paper.

Table 3.

Periodic analysis results of pseudo light curves.

ObjectNdetPdet* (s)
pseudo 2020 HT714111.3086 ± 0.0001
pseudo 2020 PY218151.32235 ± 0.00002
pseudo 2020 TD84341.2302 ± 0.0001
pseudo 2021 CA622191.301436 ± 0.000007
pseudo 2021 CC711091.501 ± 0.001
pseudo 2021 CG18571.3906 ± 0.0002
pseudo 2021 GQ1011671.20683 ± 0.00004
pseudo 2021 TY1420511.27431 ± 0.00006
ObjectNdetPdet* (s)
pseudo 2020 HT714111.3086 ± 0.0001
pseudo 2020 PY218151.32235 ± 0.00002
pseudo 2020 TD84341.2302 ± 0.0001
pseudo 2021 CA622191.301436 ± 0.000007
pseudo 2021 CC711091.501 ± 0.001
pseudo 2021 CG18571.3906 ± 0.0002
pseudo 2021 GQ1011671.20683 ± 0.00004
pseudo 2021 TY1420511.27431 ± 0.00006
*

Pdet is the detectable rotational period of the object with the same observational conditions in this paper.

4.2 Deficiency of fast rotators

We found no NEOs with rotational periods shorter than 10 s other than 2020 HS7. The distribution of the Tomo-e NEOs in the D–P relation is truncated around 10 s in the rotational period, as shown in figure 7. To interpret this flat-top distribution, we consider the evolution of rotational periods of the NEOs.

Since smaller asteroids experience a stronger Yarkovsky effect and their semi-major axes are changed, parts of them drift to the resonances with giant planets in the main belt in a short time scale (∼a few Myr) and then are scattered into the near-Earth region (Bottke et al. 2006). The orbits of the scattered asteroids evolve to those of NEOs over a few Myr (Gladman et al. 1997). Therefore, typical NEOs are considered to be a few to 10 Myr old. This timescale (hereinafter referred to as NEO age) is consistent with the typical cosmic ray exposure age of meteorites (Eugster et al. 2006).

Since YORP gradually changes the rotational states of NEOs during the orbital evolution, the distribution of the rotational periods reflects the NEO age. Although YORP also decelerates the rotation, here we consider only the acceleration. The decelerated tiny asteroids shortly enter tumbling states once spinning down starts (Vokrouhlický et al. 2007; Breiter et al. 2011) and it is difficult to predict their evolution accurately. In this study, we estimate reachable rotational periods of NEOs by the YORP acceleration. For the sake of the simplicity, we do not take into account the time evolution of the orbital elements, resulting in a constant acceleration.

We use two assumptions as follows. A tiny asteroid is a fragment of a collisional event and its initial rotational period, Pinit, is given by an extrapolation of the diameter and rotational period relation for millimeter-sized fragments in a collisional experiment (Kadono et al. 2009):
(11)
The YORP acceleration follows a scaling law and is derived from the YORP strength of the near-Earth object Bennu (Vokrouhlický et al. 2004; Hergenrother et al. 2019):
(12)
where ω is the angular velocity of the asteroid, DBennu is the diameter of Bennu, aBennu and aast are the semi-major axes of Bennu and the asteroid, and eBennu and east are the orbital eccentricities of Bennu and the asteroid. We adopt a DBennu of 482 m, aBennu of 1.126 au, and eBennu of 0.204 (JPL Small-Body Database).5 We set aast to 2 au and east to zero since most NEOs have come from the inner main belt (Granvik et al. 2018).
We assume a linear acceleration of a rotational period by YORP and obtain the ω in time t as follows:
(13)
where ω0 is the initial angular velocity of the asteroid. We calculate the NEO age, τYORP, as follows by solving equation (13) for t with equations (11) and (12):
(14)

Figure 12 shows isochrones for t = 0.1, 1, 10, 100, and 1000 Myr. Based on the isochrones, tiny NEOs with diameters less than 10 m and ages older than 10 Myr, corresponding to the typical dynamical evolution timescale of the NEOs, rotates faster than about 10 s. However, no such fast rotators are found, other than 2020 HS7. The observed truncation is not produced by the constant acceleration model.

The densities and surface properties of NEOs depend on their sizes (Carry 2012). However, the density difference of NEOs is a factor of a few at most and does not suppress the acceleration of rotation sufficiently. The thermal inertia also has little effect on the rotational period (Čapek & Vokrouhlický 2004; Golubov et al. 2021). Therefore, other dynamical mechanisms are required to explain the flat-top distribution.

4.2.1 Tensile strength

We discuss the possibility that fast-rotating tiny asteroids are destroyed by the centrifugal force. The critical rotational period for keeping the shape against the centrifugal force, Pcri, is expressed as follows:
(15)
where ρ is a bulk density and κ is a tensile strength coefficient (Holsapple 2007; Kwiatkowski et al. 2010). Cshape is the coefficient indicating the shape of the asteroid, defined as
(16)
where C1 and C2 are the axial ratios of c/a and b/a, respectively, and Cfric is a friction coefficient (Holsapple 2007). We adopt a C1 of 0.7, C2 of 0.7, and Cfric of 0.31, corresponding to a friction angle of 40°. Then, the shape coefficient Cshape equals 1.8.

We present two lines indicating Pcri with tensile strength of typical stony meteorites (κ = 105 N m−3/2, Kwiatkowski et al. 2010) and weak material (κ = 103 N m−3/2), respectively, in panel (b) of figure 12. We use a typical density of S-type asteroids (ρ = 2500 kg m−3). In the case of weak material, we can explain the deficiency of NEOs with D ≤ 10 m and P ≤ 10 s. However, the flat-top shape of the distribution is not reproduced because Pcri is proportional to D5/4.

4.2.2 Suppression of YORP by meteoroid impacts

The YORP acceleration can be suppressed by meteoroid impacts on to an asteroid surface (Farinella et al. 1998; Wiegert 2015). We investigate the evolution of the rotational period taking into account possible effects by meteoroid impacts. We discuss two effects related to meteoroid impacts: angular momentum transfer and cratering.

4.2.2.1 Angular momentum transfer

The absolute angular momentum of an asteroid is written as L = Iω, where I is a moment of inertia of the asteroid. A change of the angular momentum caused by a collision of a meteoroid is expressed as |$\delta L = \beta |m \boldsymbol {v}_{\mathrm{imp}}\times \boldsymbol {R}|$|⁠, where β is a dimensionless momentum multiplication factor, m is the mass of the meteoroid, |$\boldsymbol {v}_{\mathrm{imp}}$| is the impact velocity vector of the meteoroid, and |$\boldsymbol {R}$| is the position vector from the center of the asteroid. Assuming the angle between |$\boldsymbol {v}_\mathrm{imp}$| and |$\boldsymbol {R}$| is 90°, the relative angular momentum change in a single collision is written as
(17)
where M and ρ are the mass and the bulk density of the asteroid, respectively (Wiegert 2015).

When a collision with a large δL/L occurs, the spin axis of the asteroid can be tilted, leading to a ceasing of the YORP acceleration. Therefore, a timescale of such a critical collision, τL, corresponds to the duration of the YORP acceleration,

Campbell-Brown and Braid (2011) estimated the flux of meteoroids from observations of sporadic meteors as
(18)
The typical timescale in which a meteoroid with mass larger than m collides with an asteroid with radius R is written as follows:
(19)

We adopt a β of 20, vimp of 3 × 104 m s−1, and ρ of 2500 kg m−3 as typical quantities. The timescale τL provides the possible fastest rotational period accelerated by YORP. We present three limiting lines for different δL/L values in panel (c) of figure 12. The YORP acceleration of smaller asteroids is more suppressed by the angular momentum transfer. However, the flat-top shape of the distribution is not reproduced because the reachable periods are proportional to D.

4.2.2.2 Cratering

When a sufficiently large fraction of an asteroid surface is covered with craters, the continuous YORP acceleration is not an appropriate assumption since YORP is sensitive to small structures (Statler 2009). To discuss the cratering effect of meteoroid impacts, we use the crater scaling law from Holsapple (1993):
(20)
where Vcrater is the volume of the crater, Y is the tensile strength of the target, and both K2 and slope μ are constants depending on the taxonomic type of the target. We refer to the material strength in Holsapple (2020):
(21)
The radius of the crater Rcrater is written as follows:
(22)
where KR is a constant which depends on the crater shape.
From equations (20)–(22), the surface area of a single crater, Scrater, is written as follows assuming a bowl-like crater:
(23)
From the equation (18), the flux density of the meteoroids colliding with the target, n, is expressed as a function of the mass of the impactor, m, and the radius of the target, R, as follows:
(24)
We can estimate the total surface of cratering area by meteoroids per unit time, |$S_{\mathrm{crater}}^{\mathrm{total}}$|⁠, as follows:
(25)

where m0 and m1 are minimum and maximum masses of the meteoroids, respectively. We set |$m_1 \rightarrow \inf$| and m0 as a free parameter.

We assume that no further YORP acceleration works once the craters cover a certain fraction of the target surface, δS/S. The timescale covering δS/S of the surface with craters, τcrater, is expressed as
(26)
where S is the entire surface area of the target.
We adopt a K2 of 1 and μ of 0.55, typical values for S-type asteroids. Assuming a bowl-like crater, we set KR to 1.3 (Holsapple 1993, 2020). The timescale for S-type asteroids, τcrater, S, is given by
(27)

We adopt a ρ of 2500 kg m−3 and vimp of 3 × 104 m s−1. The possible fastest rotational periods are presented over a wide range of m0 values in panel (d) of figure 12. The possible fastest rotational period is approximately proportional to D. Therefore, we cannot explain the truncated distribution with the suppression of YORP by cratering.

4.2.3 Tangential YORP effect

We have considered only the normal YORP (NYORP), disregarding tangential YORP (TYORP). TYORP depends on the rotational period and thermal properties of the asteroid, as with NYORP. In most cases, TYORP contributes to the acceleration of the rotation unlike NYORP, which decelerates the rotation as well (Golubov & Kruguly 2012; Golubov et al. 2014).

By taking both NYORP and TYORP into consideration, the YORP acceleration is expressed as follows:
(28)
where γ is the fraction of the NYORP contribution to the total YORP strength, η(θ) is the efficiency function of TYORP, and θ is the thermal parameter corresponding to a ratio of two characteristic scales related to thermal conductivity: the thermal conductivity length Lcond and the length of the heat conductivity wave Lwave (Golubov & Kruguly 2012).
The thermal conductivity length is defined as
(29)
where λ is the heat conductivity of the asteroid, ϵ and A are the thermal emissivity and the Bond albedo of the surface, respectively, Φ is the solar energy flux, and σ is Stefan–Boltzmann’s constant. Lcond is a typical scale of how far the heat conduction extends. The length of the heat conductivity wave is defined as
(30)
where C is the heat capacity of the asteroid. Lwave is a typical scale of how far the heat is transferred when considering a time variation against a heat source.
Therefore, θ is written as follows:
(31)
The parameter θ characterizes the temperature condition of the surface and is a function of a rotational period.
Numerical simulations show that the TYORP effect is significant for θ ∼ 1 (Golubov & Kruguly 2012; Golubov et al. 2014). We simplify the efficiency of TYORP as follows:
(32)
where θmin and θmax are free parameters. The isochrones considering TYORP are shown in panel (a) of figure 13. We adopt γ of 0.1 and 0.5 since TYORP is thought to be as strong as or stronger than NYORP (Golubov & Kruguly 2012; Golubov et al. 2014). Previous studies suggest that parts of tiny NEOs have fine particles on the surface (Mommert et al. 2014; Fenucci et al. 2021). We assume that the asteroid surface is covered by regolith with λ = 0.0015 W m−1 K−1, C = 680 J kg−1 K−1, and ρ = 1500 kg m−3. We set ϵ = 0.7 and a = 2.0 au corresponding to typical values for NEOs. We adopt A = 0.084, which is derived with typical properties of moderate albedo asteroids: pV of 0.2 and a phase integral q of 0.42 (Shevchenko et al. 2019). As of 2021 November, the change of the rotational periods of 10 asteroids has been confirmed (Ďurech et al. 2022, and references therein). The range of θ among the 10 asteroids is calculated to be from 0.26 to 1.3. Since all 10 asteroids are accelerated, not decelerated, we assume that TYORP is effective for all of them. Thus, we set θmin and θmax to 0.1 and 5, respectively. The YORP acceleration considering TYORP successfully leads to flat-top shapes around D ∼ 100 m and P ∼ 300 s since the YORP acceleration becomes weaker at θ = θmax = 5. However, they do not match the truncated distribution around D ∼ 10 m and P ∼ 10 s seen in the D–P relation diagram. In the case of θmax = 30, the isochrones become similar to the observed distribution as shown in panel (b) of figure 13. The larger θ value means that many more asteroids experience TYORP acceleration than theoretically predicted. The fact that TYORP acts up to θ = 30 under the assumptions above is rephrased as the asteroids being illuminated by stronger radiation or thermal parameters such as C and λ being smaller. Most Tomo-e NEOs have perihelion distances smaller (r ∼ 1 au) than 2 au at the time of observations. Thus, in the case of C or λ being an order of magnitude less, θ changes by a factor of (22)3/4 × (10)1/2 ∼ 9. The observed truncation around 10 s in rotational period may be produced by the TYORP effect.

5 Conclusions

The rotational period of an asteroid reflects its dynamical history and physical properties. We have obtained the light curves of 60 tiny (diameter less than 100 m) NEOs with the wide-field CMOS camera Tomo-e Gozen. We successfully derived the rotational periods and axial ratios of 32 samples owing to the video observations at 2 fps. We found 13 objects with rotational periods less than 60 s. Compared with the literature, the distribution of the rotational periods of 32 objects shows a potential excess in shorter periods. This result suggests that previous studies missed some population of fast-rotating asteroids due to long exposure time observations.

We discovered that the distribution of the tiny NEOs in the D–P diagram is truncated around a period of 10 s. We performed model calculations taking into account the YORP effect. A NEO smaller than 10 m is expected to rotate with a period shorter than 10 s assuming a constant acceleration by YORP, which is not consistent with the present results. The truncated distribution is not well explained by either the realistic tensile strength of NEOs or the suppression of YORP by meteoroid impacts. We found that the tangential YORP effect is a possible mechanism to produce the truncated distribution, although further observational and theoretical studies as well as high-speed light curve observations of NEOs are necessary to reach the conclusion.

Acknowledgements

We give special thanks to Mr. Yuto Kojima for his technical assistance with this study. We would like to thank near-Earth asteroid observers around the world. J.B. would like to express the gratitude to the Iwadare Scholarship Foundation and the Public Trust Iwai Hisao Memorial Tokyo Scholarship Fund for the grants. This work has been supported by the Japan Society for the Promotion of Science (JSPS) KAKENHI grants, 21H04491, 20H04617, 18H05223, 18H01272, 18H01261, 18K13599, 17H06363, 16H06341, 16H02158, 26247074, and 25103502. This work is supported in part by the Optical and Near-Infrared Astronomy Inter-University Cooperation Program, the Ministry of Education, Culture, Sports, Science and Technology (MEXT) of Japan, JST SPRING, Grant Number JPMJSP2108, and the UTEC UTokyo Scholarship. This work has made use of data from the European Space Agency (ESA) mission Gaia 〈https://www.cosmos.esa.int/gaia〉, processed by the Gaia Data Processing and Analysis Consortium (DPAC, https://www.cosmos.esa.int/web/gaia/dpac/consortium). Funding for the DPAC has been provided by national institutions, in particular the institutions participating in the Gaia Multilateral Agreement.

Appendix. Light curves, periodograms, and phased light curves

Light curves, Lomb–Scargle periodograms, and phased light curves of the Tomo-e NEOs are presented here in figures 1416.

Footnotes

4

Barbary, K., Boone, K., & Deil, C. 2015, sep: v1.3.0, doi:10.5281/zenodo.15669.

5

https://ssd.jpl.nasa.gov/tools/sbdb_lookup.html〉, last accessed 2021-12-20.

References

Akaike
 
H.
 
1974
,
IEEE Trans. Automatic Control
,
19
,
716

Bertin
 
E.
,
Arnouts
 
S.
 
1996
,
A&AS
,
117
,
393

Birtwhistle
 
P.
 
2021a
,
Minor Planet Bull.
,
48
,
180

Birtwhistle
 
P.
 
2021b
,
Minor Planet Bull.
,
48
,
286

Birtwhistle
 
P.
 
2021c
,
Minor Planet Bull.
,
48
,
341

Bottke
 
W. F.
,
Jedicke
 
R.
,
Morbidelli
 
A.
,
Petit
 
J.-M.
,
Gladman
 
B.
 
2000
,
Science
,
288
,
2190

Bottke
 
W. F.
,
Vokrouhlický
 
D.
,
Rubincam
 
D. P.
,
Nesvorný
 
D.
 
2006
,
Annu. Rev. Earth Planet. Sci.
,
34
,
157

Bowell
 
E.
,
Hapke
 
B.
,
Domingue
 
D.
,
Lumme
 
K.
,
Peltoniemi
 
J.
,
Harris
 
A. W.
 
1989
, in
Asteroids II
, ed.
Binzel
 
R. P.
 et al.
(
Tucson
:
University of Arizona Press
),
524

Breiter
 
S.
,
Rożek
 
A.
,
Vokrouhlický
 
D.
 
2011
,
MNRAS
,
417
,
2478

Campbell-Brown
 
M. D.
,
Braid
 
D.
 
2011
, in
Meteoroids: The Smallest Solar System Bodies
, ed.
Cooke
 
W. J.
 et al.
(
Huntsville, AL
:
National Aeronautics and Space Administration
),
304

Čapek
 
D.
,
Vokrouhlický
 
D.
 
2004
,
Icarus
,
172
,
526

Carry
 
B.
 
2012
,
Planet. Space Sci.
,
73
,
98

Chambers
 
K. C.
 et al.  
2016
,
arXiv:1612.05560

Drake
 
A. J.
 et al.  
2009
,
ApJ
,
696
,
870

Ďurech
 
J.
 et al.  
2022
,
A&A
,
657
,
A5

Eugster
 
O.
,
Herzog
 
G. F.
,
Marti
 
K.
,
Caffee
 
M. W.
 
2006
,
Irradiation Records, Cosmic-Ray Exposure Ages, and Transfer Times of Meteorites
, ed.
Lauretta
 
D. S.
,
McSween
 
H. Y.
(
Tucson
:
University of Arizona Press
),
829

Farinella
 
P.
,
Vokrouhlický
 
D.
,
Hartmann
 
W. K.
 
1998
,
Icarus
,
132
,
378

Fenucci
 
M.
,
Novaković
 
B.
,
Vokrouhlický
 
D.
,
Weryk
 
R. J.
 
2021
,
A&A
,
647
,
A61

Fowler
 
J. W.
,
Chillemi
 
J. R.
 
1992
,
Phillips Lab. Tech. Rep.
,
2049
,
17

Gaia Collaboration  

2018
,
A&A
,
616
,
A1

Ginsburg
 
A.
 et al.  
2019
,
AJ
,
157
,
98

Gladman
 
B. J.
 et al.  
1997
,
Science
,
277
,
197

Golubov
 
O.
,
Krugly
 
Y. N.
 
2012
,
ApJ
,
752
,
L11

Golubov
 
O.
,
Scheeres
 
D. J.
,
Krugly
 
Y. N.
 
2014
,
ApJ
,
794
,
22

Golubov
 
O.
,
Unukovych
 
V.
,
Scheeres
 
D. J.
 
2021
,
AJ
,
162
,
8

Granvik
 
M.
 et al.  
2018
,
Icarus
,
312
,
181

Hatch
 
P.
,
Wiegert
 
P. A.
 
2015
,
Planet. Space Sci.
,
111
,
100

Hergenrother
 
C. W.
 et al.  
2019
,
Nature Commun.
,
10
,
1291

Holsapple
 
K. A.
 
1993
,
Annu. Rev. Earth Planet. Sci.
,
21
,
333

Holsapple
 
K. A.
 
2007
,
Icarus
,
187
,
500

Holsapple
 
K. A.
 
2020
,
arXiv:2012.15300

Kadono
 
T.
,
Arakawa
 
M.
,
Ito
 
T.
,
Ohtsuki
 
K.
 
2009
,
Icarus
,
200
,
694

Kojima
 
Y.
 et al.  
2018
,
Proc. SPIE
,
10709
,
107091T

Kwiatkowski
 
T.
 et al.  
2021
,
A&A
,
656
,
A126

Kwiatkowski
 
T.
,
Polinska
 
M.
,
Loaring
 
N.
,
Buckley
 
D. A. H.
,
O’Donoghue
 
D.
,
Kniazev
 
A.
,
Romero Colmenero
 
E.
 
2010
,
A&A
,
511
,
A49

Lomb
 
N. R.
 
1976
,
Ap&SS
,
39
,
447

Michikami
 
T.
 et al.  
2019
,
Icarus
,
331
,
179

Michikami
 
T.
,
Nakamura
 
A. M.
,
Hirata
 
N.
 
2010
,
Icarus
,
207
,
277

Mommert
 
M.
 et al.  
2014
,
ApJ
,
789
,
L22

Ohsawa
 
R.
 
2021
,
J. Space Sci. Informatics Japan
,
11
,
1

Paolicchi
 
P.
,
Burns
 
J. A.
,
Weidenschilling
 
S. J.
 
2002
,
Asteroids III
, ed.
Bottke
 
W. F.
 Jr.
 et al.
(
Tucson
:
University of Arizona Press
),
517

Pravec
 
P.
 et al.  
2005
,
Icarus
,
173
,
108

Pravec
 
P.
,
Harris
 
A. W.
 
2000
,
Icarus
,
148
,
12

Pravec
 
P.
,
Harris
 
A. W.
 
2007
,
Icarus
,
190
,
250

Rubincam
 
D. P.
 
2000
,
Icarus
,
148
,
2

Sako
 
S.
 et al.  
2018
,
Proc. SPIE
,
10702
,
107020J

Scargle
 
J. D.
 
1982
,
ApJ
,
263
,
835

Shevchenko
 
V. G.
 et al.  
2019
,
A&A
,
626
,
A87

Statler
 
T. S.
 
2009
,
Icarus
,
202
,
502

Thirouin
 
A.
 et al.  
2016
,
AJ
,
152
,
163

Thirouin
 
A.
 et al.  
2018
,
ApJS
,
239
,
4

Tonry
 
J. L.
 et al.  
2018
,
PASP
,
130
,
064505

VanderPlas
 
J. T.
 
2018
,
ApJS
,
236
,
16

Vokrouhlický
 
D.
 
1998
,
A&A
,
335
,
1093

Vokrouhlický
 
D.
,
Breiter
 
S.
,
Nesvorný
 
D.
,
Bottke
 
W. F.
 
2007
,
Icarus
,
191
,
636

Vokrouhlický
 
D.
,
Čapek
 
D.
 
2002
,
Icarus
,
159
,
449

Vokrouhlický
 
D.
,
Čapek
 
D.
,
Kaasalainen
 
M.
,
Ostro
 
S. J.
 
2004
,
A&A
,
414
,
L21

Vokrouhlický
 
D.
,
Milani
 
A.
,
Chesley
 
S. R.
 
2000
,
Icarus
,
148
,
118

Warner
 
B. D.
,
Harris
 
A. W.
,
Pravec
 
P.
 
2009
,
Icarus
,
202
,
134

Wiegert
 
P. A.
 
2015
,
Icarus
,
252
,
22

Yeomans
 
D. K.
 et al.  
2000
,
Science
,
289
,
2085

Zappala
 
V.
,
Cellino
 
A.
,
Barucci
 
A. M.
,
Fulchignoni
 
M.
,
Lupishko
 
D. F.
 
1990
,
A&A
,
231
,
548

Zhai
 
C.
 et al.  
2014
,
ApJ
,
792
,
60

This is an Open Access article distributed under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0/), which permits unrestricted reuse, distribution, and reproduction in any medium, provided the original work is properly cited.