A satellite of mass m, is orbiting around the earth at a distance r from centre of earth, if it stopped suddenly the loss in total energy will be
The minimum energy required to launch a satellite of mass m from the surface of earth of radius R in a cirulcar orbit at an altitude 2R is (mass of earth is M)
A body of mass m is kept at a small height h above the ground. If the radius of the earth is R and its mass is M, the potential energy of the body and earth system (with h = ∞ being the reference position) is