MCQ
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
- ✓$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}}}} $
