\begin{table}%t4 \caption{\label{tab:orbitalelements}Orbital elements as determined with the algorithm from \citet{doc85} and our grid search algorithm (described in Sect.~\ref{sec:orbitsolution}). } %\centerline { \begin{tabular}{ll|cc} \hline\hline & & Docobo & Grid search \\ Parameter & & algorithm & algorithm \\ \hline $P$ & [yrs] & $11.05 \pm 0.03$ & $11.26 \pm 0.5$ \\ $T_{0}$ & & $2002.87 \pm 0.40$ & $2002.57 \pm 0.5$ \\ $e$ & & $0.534 \pm 0.050$ & $0.592 \pm 0.07$ \\ $a$ & [mas] & $40.00 \pm 3.00$ & $43.61 \pm 3$ \\ $i$ & [\degr] & $100.7 \pm 1.0$ & $99.0 \pm 2.6$ \\ $\Omega$ & [\degr] & $25.3 \pm 1.5$ & $26.5 \pm 1.7$ \\ $\omega$ & [\degr] & $290.9 \pm 2.5$ & $285.8 \pm 8.5$ \\ $\chi^2_r$ & & 1.84 & 0.56 \\%[-3.2mm]\\ \hline%\\[-3.2mm] $a^{3}/P^{2}$ & [mas$^3$/yrs$^2$] & $524 \pm 130$ & $645 \pm 200$ \\ $M_{\rm C1}/M_{\rm C2}$ & & $0.21 \pm 0.05$ & $0.23 \pm 0.05$ \\ $M_{\rm C1}+M_{\rm C2}$ & [$M_{\odot}$] & $49 \pm 4$ & $47 \pm 4$ \\ $d_{\rm dyn}$ & [pc] & $456 \pm 13$ & $416 \pm 12$ \\ \hline \end{tabular}} \par \medskip {Notes}. Besides the orbital elements, we give the mass ratio (Sect.~\ref{sec:massratio}), dynamical distance, and system mass (Sect.~\ref{sec:dynmassparallax}), derived from both set of orbit elements. The dynamical distance and system mass was determined using the method from \citet[][method~{\it c} in Sect.~\ref{sec:dynmassparallax}]{bai46} and three different MLRs. When assuming another distance~$d^{\prime}$, the dynamical system mass $M_{\rm C1}+M_{\rm C2}$ must be scaled by a factor $(d^{\prime}/d_{\rm dyn})^3$. The mass ratio $M_{\rm C1}/M_{\rm C2}$ was also computed for the distance $d_{\rm dyn}$, but can be converted to any other distance using Eq.~(\ref{eqn:massratio}). \end{table}