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Table 6
The eccentric-orbit solutions for the subsets of automatically measured Hα emission-wing RVs.
| N s | e | ω | K 1 | L–S | N |
| (°) | (km s-1) | test | |||
|
|
|||||
| 2 | 0.30 ± 0.14 | 322 ± 24 | 4.57 ± 0.81 | 0.174 | 24 |
| 4 | 0.42 ± 0.11 | 285 ± 17 | 5.82 ± 0.78 | 0.004 | 44 |
| 5 | 0.34 ± 0.10 | 6 ± 20 | 4.74 ± 0.62 | 0.014 | 25 |
| 7 | 0.16 ± 0.12 | 87 ± 49 | 6.0 ± 1.1 | 0.311 | 52 |
| 9 | 0.15 ± 0.19 | 92 ± 53 | 3.38 ± 0.50 | 0.583 | 40 |
| 10 | 0.098 ± 0.050 | 48 ± 23 | 4.12 ± 0.19 | 0.147 | 60 |
| 12 | 0.40 ± 0.21 | 336.0 ± 9.5 | 5.9 ± 1.2 | 0.054 | 36 |
| 13 | 0.21 ± 0.14 | 82 ± 44 | 3.94 ± 0.53 | 0.157 | 59 |
| 14 | 0.167 ± 0.068 | 111 ± 20 | 4.57 ± 0.33 | 0.026 | 46 |
| 16 | 0.26 ± 0.13 | 227 ± 24 | 4.61 ± 0.56 | 0.201 | 27 |
Notes. Ns = a number of a RV subset (the same numbering being also used in Fig. 9), L–S test = probability that the eccentricity found is false, N = number of RVs in the subset.
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