A satellite of mass 'm' is revolving in circular orbit of radius 'r' round the earth. Its angular momentum w.r.t. the centre of its orbit is (M= mass of earth, G= universal gravitational constant)
(GMmr)12
(GMm2r)12
(GMm2r2)12
(GM2m2r)12
A
(GMm2r)12
B
(GMmr)12
C
(GM2m2r)12
D
(GMm2r2)12
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