
The orbital velocity of an artificial satellite in a circular orbit just above the centre’s surface is v.
For a satellite orbiting at an altitude of half of the earth’s radius, the orbital velocity is
(A) 3v/2 (B) 3 / 2v
(C) 2 / 3 v (D) (2/3)v
For a satellite orbiting at an altitude of half of the earth’s radius, the orbital velocity is
(A) 3v/2 (B) 3 / 2v
(C) 2 / 3 v (D) (2/3)v




