1.The ratio of energy required to raise a satellite to a height hhh above the earth's surface to that required to put it into the orbit at the same height is (RRR = radius of earth):a.2hR+h\frac{2h}{R+h}R+h2hb.hR+2h\frac{h}{R+2h}R+2hhc.RR+h\frac{R}{R+h}R+hRd.R+h2R\frac{R+h}{2R}2RR+hLogin to continueOnly logged in users canattempt or see the solution.