The ratio of energy required to raise a satellite to a height h above the earth's surface to that required to put it into the orbit is

E1 = ∆U = mgh1+h/RE2 = Energy of satellite-Energy of sateilite on surface of earth=-GMm2(R+h)+GMmR=mgR1-12(1+h/R)  ∵GM=gR2⇒  E2=mgR2hR+121+hR∴  E1E2=mgh1+hR×21+hRmgR=2hR  ∵h<