An Earth-orbiting research satellite of mass 500kg is initially in a circular orbit 300km above Earth’s surface. It is raised to a new circular orbit 1000km above the surface. How much work must be done on the satellite to accomplish this change in orbit? (Take Earth’s radius to be 6.37×106m and GME=3.99×1014m3/s2.)
(a) 3.4×109J
(b) 9.0×108J
(c) 1.4×109J
(d) 2.9×109J