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Table 4
Best fitted orbital solution using the direct n-body equations of motion, and adopting the orbital parameters listed in Table 3 as the starting point.
| Tadpole | ||
| param. | planet 1 | planet 2 |
|
|
||
| m [M⊕] | 195.68 ± 0.31 | 100.40 ± 0.35 |
| a [au] | 0.099 ± 6 × 10-5 | 0.101 ± 1 10-4 |
| λ [deg] | 2.3 ± 1.7 | 306 ± 5 |
| e | 0.056 ± 0.003 | 0.049 ± 0.003 |
| ϖ [deg] | 0.01 ± 0.04 | 304.2 ± 0.4 |
| I [deg] | 65 ± 2 | 57 ± 3 |
|
|
||
 [au] |
0.09953 | |
| ζ0 [deg] | 37.40 | |
| δ | 0.3391 | |
|
|
||
|
1.652 | |
| rms[m s-1] | 1.8770 | |
| horseshoe | ||
| param. | planet 1 | planet 2 |
|
|
||
| m [M⊕] | 18.79 ± 0.008 | 2.99 ± 0.005 |
| a [au] | 0.100 ± 2 × 10-5 | 0.099 ± 7 10-5 |
| λ [deg] | 4.69 ± 2.83 | 318.42 ± 8.56 |
| e | 0.000 ± 10-3 | 0.000 ± 10-3 |
| ϖ [deg] | 0.000 ± 10-3 | 0.000 ± 10-3 |
| I [deg] | 90* | 90* |
|
|
||
| [au] |
0.1000 | |
| ζ0 [deg] | 21.57 | |
| δ | 0.1371 | |
|
|
||
|
|
1.595 | |
| rms[m s-1] | 1.8513 | |
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