A satellite of mass m is circulating around the earth with constant angular velocity. If radius of the orbit is \[{{R}_{0}}\] and mass of the earth M, the angular momentum about the centre of the earth is [MP PMT 1996; RPMT 2000]

• A.             \[m\sqrt{GM{{R}_{0}}}\]
• B.               \[M\sqrt{Gm{{R}_{0}}}\]
• C.             \[m\sqrt{\frac{GM}{{{R}_{0}}}}\] 
• D.             \[M\sqrt{\frac{GM}{{{R}_{0}}}}\]