The satellite of mass m is moving in a circular orbit of radius r. ∴ Kinetic energy of the satellite, K=2rGMm .....(i) Potential energy of the satellite, U=r−GMm ....(ii) Orbital speed of satellite, v=rGM ....(iii) Time-period of satellite, T=[(GM4π2)r3t]1/2 .....(iv) Given mS1=4mS2 since M,r is same for both the satellites S1 and S2∴ From equation (ii), we get U∝m∴US2US1=mS2mS1=4 or, US1=4US2 Option (a) is wrong. From (iii), since v is independent of the mass of a satellite, the orbital speed is same for both satellites S1 and S2 Hence option (b) is correct. From (i), we get K∝m∴KS2KS1=mS2mS1=4 or, KS1=4KS2 Hence option (c) is wrong. From (iv), since T is independent of the mass of a satellite, time period is same for both the satellites S1 and S2. Hence option(d) is wrong.