Table 3.

Maximum and minimum eccentricity (equations 31 and 32) for each type of compact object. The values of emin and emax are obtained for θ = 0.1 rad (prograde orbits), θ = −0.1 rad (retrograde orbits), acrit = aRQ, MMBH = 4.3 × 106 M, and a = 0 or 0.999.

a = 0.0
Objecteminemax
BD0.9631780.998160
WD0.9819570.999790
NS0.9972680.999919
BH0.9967910.999971
a = 0.999
ProgradeRetrograde
eminemaxeminemax
BD0.9906050.9999540.9474890.995773
WD0.9953960.9999950.9742700.999505
NS0.9993030.9999980.9961040.999810
BH0.9991810.9999990.9954240.999932
a = 0.0
Objecteminemax
BD0.9631780.998160
WD0.9819570.999790
NS0.9972680.999919
BH0.9967910.999971
a = 0.999
ProgradeRetrograde
eminemaxeminemax
BD0.9906050.9999540.9474890.995773
WD0.9953960.9999950.9742700.999505
NS0.9993030.9999980.9961040.999810
BH0.9991810.9999990.9954240.999932
Table 3.

Maximum and minimum eccentricity (equations 31 and 32) for each type of compact object. The values of emin and emax are obtained for θ = 0.1 rad (prograde orbits), θ = −0.1 rad (retrograde orbits), acrit = aRQ, MMBH = 4.3 × 106 M, and a = 0 or 0.999.

a = 0.0
Objecteminemax
BD0.9631780.998160
WD0.9819570.999790
NS0.9972680.999919
BH0.9967910.999971
a = 0.999
ProgradeRetrograde
eminemaxeminemax
BD0.9906050.9999540.9474890.995773
WD0.9953960.9999950.9742700.999505
NS0.9993030.9999980.9961040.999810
BH0.9991810.9999990.9954240.999932
a = 0.0
Objecteminemax
BD0.9631780.998160
WD0.9819570.999790
NS0.9972680.999919
BH0.9967910.999971
a = 0.999
ProgradeRetrograde
eminemaxeminemax
BD0.9906050.9999540.9474890.995773
WD0.9953960.9999950.9742700.999505
NS0.9993030.9999980.9961040.999810
BH0.9991810.9999990.9954240.999932
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