\begin{table}
%\begin{center}
\par
\caption{Satellite orbital elements and physical parameters used
in the numerical simulations.}\label{T-sat}
\begin{tabular}{lcccc} \hline\hline
 & Mab & Puck & Rosalind & Portia \\
\hline
$a$ (km) & 97~735 & 86~004 & 69~926 & 66~097 \\
$e$ ($\times10^{-3}$) & 2.54 & 0.39 & 0.58 & 0.51 \\
$i$ ($^\circ$) & 0.134 & 0.321 & 0.093 & 0.18 \\
$\omega$ ($^\circ$) & 240.30& 331.88& 257.28 & 84.41 \\
$\Omega$ ($^\circ$) & 350.74& 199.48& 157.64 & 77.71 \\
$r$ (km) & 12 & 81 & 36 & 70 \\ \hline
\end{tabular}
%\end{center}
\par
\end{table}