Open Access
Table A.6.
Orbital elements from moderately certain combined dynamical and LTTE solutions for systems.
KIC No. | P1 | P2 | a2 | e2 | ω2 | τ2 | f(mC) |
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mAB | mC |
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---|---|---|---|---|---|---|---|---|---|---|---|
(day) | (day) | (R⊙) | (deg) | (MBJD) | (M⊙) | (M⊙) | (M⊙) | ||||
5080652 | 4.14435547(8) | 222.9(5) | 251(28) | 0.15(5) | 350(7) | 54865(15) | 0.50(44) | 0.49(15) | 2.18(45) | 2.10(133) | 0.89 |
6877673 | 36.7593121(8) | 3765(48) | 1268(11) | 0.18(1) | 158(2) | 53869(39) | 0.0134(4) | 0.193(2) | 1.56(1) | 0.37(1) | 1.9 |
7837302 | 23.836787(2) | 1381.3(9) | 720(13) | 0.265(8) | 155(7) | 56346(7) | 0.010(2) | 0.16(2) | 2.20(13) | 0.42(5) | 7.1 |
9664215 | 3.3195332(1) | 928(2) | 537(18) | 0.55(2) | 182(3) | 55758(6) | 0.14(2) | 0.39(1) | 1.49(20) | 0.93(14) | 0.45 |
5470(65) | 321(31)a | 0.40(7) | 254(16) | 56414(252) | 0.015(4) | − | 0.57a | 3: | |||
10268809 | 24.708843(5) | 4084(6) | 1473(27) | 0.636(6) | 290(2) | 56144(4) | 0.17(2) | 0.41(1) | 1.52(11) | 1.05(9) | 4.61 |
10296163 | 9.29678473(3) | 3408(3) | 1274(68) | 0.385(6) | 2.6(8) | 55953(5) | 0.0036(8) | 0.142(6) | 2.05(38) | 0.34(6) | 0.31 |
12356914 | 27.308390(3) | 1824(6) | 942(15) | 0.384(9) | 106(3) | 55863(8) | 0.0052(5) | 0.135(5) | 2.92(15) | 0.46(3) | 7.8 |
Notes. (a)The fourth-body orbit is a pure LTTE solution; hence, the given value is aABCsin i3 instead of a3 and, similarly, instead of mD, what is given is its minimum mass (for i3 = 90°).
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