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Match Column-I with Column-II. For a satellite in
P
circular orbit.
\begin{tabular}{|l|l|l|l|}
\hline \multicolumn{2}{|c|}{ Column-I } & \multicolumn{2}{c|}{ Column-II } \\
\hline (A) & Kinetic energy & (P) & \( -\frac{G M_{E} m}{2 r} \) \\
\hline (B) & Potential energy & (Q) & \( \sqrt{\frac{G M_{E}}{r}} \) \\
\hline (C) & Total energy & (R) & \( -\frac{G M_{E} m}{r} \) \\
\hline (D) & Orbital velocity & (S) & \( \frac{G M_{E} m}{2 r} \) \\
\hline
\end{tabular}

Codes:
\begin{tabular}{lllll}
& A & B & C & D \\
(1) & \( \mathrm{R} \) & \( \mathrm{S} \) & \( \mathrm{Q} \) & \( \mathrm{P} \) \\
(2) & \( \mathrm{Q} \) & \( \mathrm{P} \) & \( \mathrm{R} \) & \( \mathrm{S} \) \\
(3) & \( \mathrm{P} \) & \( \mathrm{Q} \) & \( \mathrm{S} \) & \( \mathrm{R} \) \\
(4) & \( \mathrm{S} \) & \( \mathrm{R} \) & \( \mathrm{P} \) & \( \mathrm{Q} \)
\end{tabular}


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