Table A.5.
Orbital elements from certain combined dynamical and LTTE solutions for systems.
| KIC No. | P1 | P2 | a2 | e2 | ω2 | τ2 | f(mC) |
 |
mAB | mC |
 |
|---|---|---|---|---|---|---|---|---|---|---|---|
| (day) | (day) | (R⊙) | (deg) | (MBJD) | (M⊙) | (M⊙) | (M⊙) | ||||
| 3544694 | 3.84572314(8) | 80.92(3) | 97(4) | 0.113(4) | 327(2) | 55723.9(4) | 0.043(8) | 0.29(1) | 1.34(20) | 0.54(8) | 4.13 |
| 4079530 | 17.727144(1) | 141.7(9) | 130(5) | 0.52(2) | 22(7) | 54987(8) | 0.000000004(1) | 0.0013(2) | 1.48(16) | 0.0020(3) | 475 |
| 4909707 | 2.30236795(4) | 515.0(3) | 489(23) | 0.59(2) | 175(3) | 54848(5) | 0.349(124) | 0.39(06) | 3.60(77) | 2.31(35) | 0.52 |
| 4940201 | 8.8165585(3) | 364.6(2) | 303(4) | 0.227(5) | 258(3) | 54868(3) | 0.10(1) | 0.33(1) | 1.88(9) | 0.94(6) | 3.06 |
| 5095269 | 18.6118308(1) | 235.89(2) | 219.32(2) | 0.072(3) | 328.4(6) | 55004.2(5) | 0.000000016(1) | 0.00192(7) | 2.28 | 0.0049(2) | 133 |
| 5255552a | 32.46529(7) | 860.1(6) | 574(7) | 0.372(2) | 40.2(4) | 54868(1) | 0.20(1) | 0.390(5) | 2.10(10) | 1.34(7) | 35 |
| 5384802 | 6.08309218(9) | 256.08(5) | 297(9) | 0.371(4) | 9(2) | 54998(2) | 0.42(6) | 0.43(1) | 3.06(39) | 2.31(32) | 4.4 |
| 5650317 | 2.14054699(2) | 118.38(2) | 182(6) | 0.20(2) | 228(7) | 55238(3) | 0.22(5) | 0.34(2) | 3.81(48) | 1.94(31) | 0.83 |
| 5653126 | 38.49130(2) | 969.4(4) | 687(5) | 0.170(3) | 322.2(8) | 54514(3) | 0.127(9) | 0.303(7) | 3.22(9) | 1.40(6) | 30 |
| 5731312 | 7.94638807(8) | 919.7(8) | 458(2) | 0.598(2) | 19(1) | 54830(1) | 0.00192(5) | 0.1082(8) | 1.36(2) | 0.165(3) | 4.69 |
| 5771589 | 10.738237(2) | 113.20(2) | 168(2) | 0.088(2) | 105(2) | 54974.8(4) | 1.25(7) | 0.634(4) | 1.81(9) | 3.14(17) | 16.8 |
| 5952403 | 0.90567813(1) | 45.468(7) | 86(2) | 0.0007(5) | 131(20) | 55506(3) | 0.75(12) | 0.57(3) | 1.81(9) | 2.35(30) | 0.036 |
| 6525196 | 3.42059731(1) | 418.90(8) | 330(5) | 0.27(1) | 92(4) | 55063(5) | 0.075(6) | 0.301(7) | 1.93(11) | 0.83(6) | 0.41 |
| 6531485b | 0.676990690(7) | 48.324(7) | 60(5) | 0.63(1) | 47(10) | 54982(2) | 0.025(8) | 0.276(8) | 0.88(28) | 0.34(11) | 4.23 |
| 6545018 | 3.99145675(2) | 90.586(3) | 106.3(8) | 0.247(5) | 233(1) | 54970.3(4) | 0.023(1) | 0.228(5) | 1.52(4) | 0.45(2) | 8.33 |
| 6546508 | 6.1071013(2) | 1235(27) | 722(35) | 0.32(3) | 318(8) | 55088(28) | 0.23(7) | 0.41(4) | 1.94(34) | 1.37(31) | 0.29 |
| 7177553 | 17.9964523(4) | 526.5(4) | 343(4) | 0.47(2) | 213(2) | 54714(2) | 0.00000012(2) | 0.0039(3) | 1.95(6) | 0.0077(6) | 39 |
| 7289157 | 5.2665486(2) | 244.1(1) | 241(6) | 0.31(1) | 163(2) | 54941(2) | 0.17(2) | 0.38(2) | 1.96(18) | 1.18(14) | 4.08 |
| 6950(424) | 426(42)c | 0.26(6) | 137(18) | 53338(409) | 0.021(6) | − | 0.66c | 3: | |||
| 7668648 | 27.82517(4) | 202.9(1) | 180(4) | 0.112(7) | 188(6) | 54931(2) | 0.018(2) | 0.213(1) | 1.51(13) | 0.41(4) | 78 |
| 7690843d | 0.78625579(4) | 74.21(3) | 157(13) | 0.48(3) | 358(2) | 54990(1) | 4.7(16) | 0.81(5) | 1.84(9) | 7.6(24) | 0.77 |
| 7812175 | 17.793579(1) | 582.0(3) | 358(14) | 0.023(2) | 220(6) | 54799(10) | 0.061(1) | 0.323(4) | 1.23(19) | 0.59(9) | 6.27 |
| 7821010 | 24.23821642(9) | 990(1) | 572(1) | 0.343(7) | 128(2) | 55122(5) | 0.000000002(0) | 0.00090(2) | 2.56(1) | 0.00229(6) | 35.3 |
| 8023317 | 16.5789557(3) | 609.9(1) | 385(11) | 0.24(2) | 165(2) | 55010(4) | 0.0006(1) | 0.067(6) | 1.92(17) | 0.14(2) | 8.31 |
| 8143170e | 28.78582(1) | 1580.5(6) | 995(9) | 0.690(6) | 107.3(4) | 54541.1(6) | 0.0081(6) | 0.123(4) | 4.64(13) | 0.65(3) | 22.2 |
| 8210721 | 22.673093(2) | 789.1(2) | 480(5) | 0.236(2) | 218.1(5) | 54634(1) | 0.082(4) | 0.325(4) | 1.61(6) | 0.78(3) | 9.90 |
| 8719897 | 3.15142051(1) | 333.30(4) | 269(8) | 0.251(4) | 130(1) | 54997.1(8) | 0.13(2) | 0.384(8) | 1.46(19) | 0.91(12) | 0.56 |
| 9007918 | 1.387206538(2) | 471.3(3) | 328(7) | 0.65(1) | 286(2) | 54818(1) | 0.00034(3) | 0.054(2) | 2.10(13) | 0.121(8) | 0.34 |
| 9451096 | 1.250390741(3) | 106.89(2) | 144(5) | 0.10(1) | 163(6) | 54994(2) | 0.046(7) | 0.24(1) | 2.65(32) | 0.84(11) | 0.19 |
| 9714358 | 6.4742284(2) | 103.76(1) | 101(1) | 0.28(1) | 119(1) | 54977.6(2) | 0.008(1) | 0.185(9) | 1.03(5) | 0.23(2) | 26.2 |
| 9850387 | 2.74849803(3) | 670.6(8) | 479(1) | 0.42(3) | 112(4) | 54690(9) | 0.019(1) | 0.180(5) | 2.72 | 0.59(2) | 0.24 |
| 10095512 | 6.0172058(1) | 472.8(2) | 334(23) | 0.18(1) | 232(6) | 54861(9) | 0.16(5) | 0.42(2) | 1.31(36) | 0.93(27) | 0.79 |
| 10223616 | 29.12926(8) | 541.9(6) | 395(14) | 0.29(3) | 239(3) | 55299.0(7) | 0.13(6) | 0.36(7) | 1.81(8) | 1.00(31) | 33 |
| 10483644 | 5.11077040(5) | 372.8(6) | 299(14) | 0.03(3) | 320(9) | 55314(7) | 0.0019(8) | 0.09(2) | 2.36(37) | 0.24(6) | 0.14 |
| 10549576 | 9.0895323(8) | 1486(4) | 1002(25) | 0.48(4) | 158(7) | 54970(32) | 0.35(7) | 0.42(3) | 3.54(25) | 2.58(38) | 0.60 |
| 10613718 | 1.17587798(2) | 88.18(5) | 129(4) | 0.11(3) | 35(17) | 54989(4) | 0.24(6) | 0.40(3) | 2.23(23) | 1.49(25) | 0.25 |
| 10979716 | 10.6840969(4) | 1046.0(6) | 602(16) | 0.470(8) | 58(2) | 54513(7) | 0.15(2) | 0.41(1) | 1.59(17) | 1.09(13) | 2.29 |
| 11519226 | 22.161754(1) | 1434(1) | 873(13) | 0.339(3) | 321.9(6) | 55010(2) | 0.33(3) | 0.43(1) | 2.50(13) | 1.84(13) | 4.90 |
Notes. (a)Quadratic and cubic ephemeris: ΔP = −5.5(2)×10−5 d/c2, c3 = 1.15(5)×10−7 d/c3. These non-linear polynomial coefficients are for the mathematical representations of additional perturbations, not considered in the analytic ETV three-body model (see Appendix B for details); (b)Quadratic ephemeris: ΔP = −1.02(2)×10−10 c/d; (c)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°); (d)Quadratic and cubic ephemeris: ΔP = 53.8(3)×10−10 d/c2, c3 = −1.49(2)×10−13 d/c3; (e)Quadratic and cubic ephemeris: ΔP = 2.4(4)×10−6 d/c2, c3 = 1.16(8)×10−8 d/c3. These non-linear polynomial coefficients are for the mathematical representations of additional perturbations, not considered in the analytic ETV three-body model (see Appendix B for details).
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.