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Table 3:

Orbital solutions deduced from different lines (Col. 1).
Line P e $\omega$ K1 $\gamma_1$ rms
  (d)   ($^\circ$) (km s-1) (km s-1) (km s-1)
H$\beta $ 4.24021 0.058 $\pm $ 0.006 140 $\pm $ 5 117.0 $\pm $ 0.5 $-29.6 \pm$ 0.6 4.9
He  II \l4686 4.24029 0.085 $\pm $ 0.003 153 $\pm $ 1 124.4 $\pm $ 0.2 $-17.3 \pm$ 0.3 2.0
He  I \l4922 4.24023 0.057 $\pm $ 0.006 148 $\pm $ 4 107.7 $\pm $ 0.4 $-17.9 \pm$ 0.5 3.8
He  I \l5015 4.24015 0.059 $\pm $ 0.006 150 $\pm $ 4 112.1 $\pm $ 0.4 $-22.2 \pm$ 0.6 4.0
He  I \l5876 4.24021 0.069 $\pm $ 0.004 151 $\pm $ 2 115.9 $\pm $ 0.3 $-22.4 \pm$ 0.4 2.9
He  I \l6678 4.24022 0.061 $\pm $ 0.005 151 $\pm $ 3 114.4 $\pm $ 0.4 $-14.7 \pm$ 0.5 3.2

The usual notations for the orbital elements have been used. Quoted uncertainties are the 1-$\sigma $ error bars.


Source LaTeX | All tables | In the text

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