\begin{table}%t1 \caption{\label{T1}Orbital parameters for the HD~60532 system $\Sa$, obtained with a 3-body Newtonian fit with $i=90^\circ$ (top) and for the system system $\Sb$, with $i=20^\circ$ (bottom) ($M_\star = 1.44~M_\odot$).} %\centering \small \begin{tabular}{l l c c} \hline \hline {\bf Param.} & {\bf [unit]} & {\bf {HD}~60532~b} & {\bf {HD}~60532~c} \\ \hline %&&& \\[-8pt] $\sqrt{\chi^2}$ & & \multicolumn{2}{c}{4.407} \\ rms & [m/s] & \multicolumn{2}{c}{4.380} \\ \hline Date & [JD-2~400~000] & \multicolumn{2}{c}{54~000.00 (fixed)} \\ $V$ & [km~s$^{-1}$] & \multicolumn{2}{c}{$ -0.0049 \pm 0.0004 $} \\ $P$ & [day] & $ 201.46 \pm 0.13 $ & $ 605.28 \pm 2.12 $ \\ $\lambda$ & [deg] & $ 14.48 \pm 0.69 $ & $ 316.23 \pm 0.95 $ \\ $e$ & & $ 0.279 \pm 0.006 $ & $ 0.027 \pm 0.007 $ \\ $\omega$ & [deg] & $ 352.15 \pm 1.08 $ & $ 136.81 \pm 16.34 $ \\ $K$ & [m/s] & $ 29.63 \pm 0.32 $ & $ 46.80 \pm 0.40 $ \\ $i$ & [deg] & $ 90 $ (fixed) & $ 90 $ (fixed) \\ \hline $M $ & [$M_\mathsf{Jup}$] & $ 1.0484 $ & $ 2.4866 $ \\ $a$ & [AU] & $ 0.7597 $ & $ 1.5822 $ \\ \hline {\bf Param.} & {\bf [unit]} & {\bf {HD}~60532~b} & {\bf {HD}~60532~c} \\ \hline &&& \\[-8pt] $\sqrt{\chi^2}$ & & \multicolumn{2}{c}{4.369} \\ rms & [m/s] & \multicolumn{2}{c}{4.342} \\ \hline Date & [JD-2~400~000] & \multicolumn{2}{c}{54~000.00 (fixed)} \\ $V$ & [km~s$^{-1}$] & \multicolumn{2}{c}{$ -0.0055 \pm 0.0003 $} \\ $P$ & [day] & $ 201.83 \pm 0.14 $ & $ 607.06 \pm 2.07 $ \\ $\lambda$ & [deg] & $ 14.78 \pm 0.66 $ & $ 317.02 \pm 0.93 $ \\ $e$ & & $ 0.278 \pm 0.006 $ & $ 0.038 \pm 0.008 $ \\ $\omega$ & [deg] & $ 352.83 \pm 1.05 $ & $ 119.49 \pm 9.14 $ \\ $K$ & [m/s] & $ 30.34 \pm 0.32 $ & $ 47.84 \pm 0.44 $ \\ $i$ & [deg] & $ 20 $ (fixed) & $ 20 $ (fixed) \\ \hline $M$ & [$M_\mathsf{Jup}$] & $ 3.1548 $ & $ 7.4634 $ \\ $a$ & [AU] & $ 0.7606 $ & $ 1.5854$ \\ \hline \end{tabular} \end{table}