How much work is required to lift a 700-kg satellite to an altitude of 3 106 m above the surface of the Earth? The gravitational force is F = GMm/r, where M is the mass of the Earth, m is the mass of the satellite, and r is the distance between the satellite and the Earth's center. The radius of the Earth is 6.4 106 m, its mass is 6 1024 kg, and in these units the gravitational constant, G, is 6.67 10-. Work = 9.96 100 J (include units; for this problem assume all given constants are accurate to many significant figures.)