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Table 5
The eccentric-orbit solutions for the subsets of manually measured Hα emission-wing RVs, shown as phase plots in Fig. 9.
| N s | e | ω | K 1 | L–S | N |
| (°) | (km s-1) | test | |||
|
|
|||||
| 2 | 0.052 ± 0.073 | 141 ± 38 | 4.30 ± 0.24 | 0.734 | 25 |
| 3 | 0.313 ± 0.082 | 165 ± 12 | 5.43 ± 0.44 | 0.001 | 42 |
| 4 | 0.416 ± 0.083 | 108.9 ± 8.3 | 6.46 ± 0.58 | 0.000 | 42 |
| 5 | 0.14 ± 0.14 | 160 ± 41 | 4.37 ± 0.60 | 0.672 | 25 |
| 7 | 0.10 ± 0.11 | 322 ± 47 | 6.88 ± 0.88 | 0.674 | 50 |
| 9 | 0.109 ± 0.067 | 201 ± 36 | 4.10 ± 0.30 | 0.299 | 42 |
| 10 | 0.120 ± 0.040 | 263 ± 16 | 5.20 ± 0.20 | 0.026 | 61 |
| 12 | 0.086 ± 0.055 | 149 ± 28 | 4.64 ± 0.26 | 0.353 | 46 |
| 13 | 0.18 ± 0.10 | 308 ± 29 | 3.56 ± 0.36 | 0.270 | 70 |
| 14 | 0.102 ± 0.040 | 147 ± 22 | 4.31 ± 0.21 | 0.038 | 59 |
| 16 | 0.116 ± 0.067 | 105 ± 31 | 3.87 ± 0.22 | 0.287 | 30 |
Notes. Ns = a number of 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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