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Table 3:

Trial solutions for the H I shell RVs, He I RVs and a combination of H$\alpha $ emission-wing RVs with He I RVs measured via cross-correlation in Jarad (1987).
Element Sol. 3 Sol. 4 Sol. 5
P (d) 132.920 133.000 132.901
  $\pm$0.013 $\pm$0.034 $\pm$0.044
$T_{\rm RV~max.}$ 47016.4 $\pm$3.6 47027.2 $\pm$3.5 47027.9 $\pm$1.3
K (km s-1) 9.74 $\pm$0.41 7.6 $\pm$1.2 8.29 $\pm$0.61
rms (km s-1) 8.09 16.25 4.44
No. of RVs 801 509 178

Solution 3 for the H I shell RVs was formally calculated as an eccentric orbit solution with e=0.25 and $\omega = 305^\circ$, the remaining two solutions are derived for a circular orbit.


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