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
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
- 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}}}} $
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