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Table 4
Eccentric-orbit solutions based on the Hα emission-wing RVs measured manually and automatically and prewhitened for the long-term changes with the program HEC13.
| Solution No.: | 1) | 2) |
| Element | Manual | Automatic |
|
|
||
| P (d) | 203.36 ± 0.10 | 203.08 ± 0.11 |
| TRVmin (RJD) | 52083 ± 17 | 52080 ± 13 |
| ω (°) | 19 ± 30 | 147 ± 22 |
| e | 0.048 ± 0.027 | 0.072 ± 0.030 |
| K1 (km s-1) | 3.88 ± 0.10 | 3.93 ± 0.12 |
| γ (km s-1) | 0.164 ± 0.071 | 0.180 ± 0.081 |
| rms (km s-1) | 1.772 | 1.948 |
| L–S test | 0.183 | 0.064 |
| No. of RVs | 757 | 700 |
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