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Table 2:

Trial circular-orbit solutions for the RVs measured on the H$\alpha $ emission wings.

Element
Sol. 1 Sol. 2
P (d) 133.036 $\pm$0.050 132.987 $\pm$0.050
$T_{\rm upper~con.}$ 47057.5 $\pm$1.8 47058.8 $\pm$1.8
$T_{\rm RV~max.}$ 47024.2 $\pm$1.8 47025.6 $\pm$1.8
K (km s-1) 6.53 $\pm$0.47 7.43 $\pm$0.46
rms (km s-1) 4.63 4.75
No. of RVs 350 341

In solution 1 long-term variations were removed via spline functions and in solution 2 using different systemic velocities of subsets.


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