A satellite of mass 1200kg orbits Earth in a circular path of radius 2RE, where RE=6.4×106m. Calculate the minimum additional work that must be done on the satellite to transfer it to a circular orbit of radius 3RE. (Take G=6.67×10−11N m2kg−2 and ME=6.0×1024kg.)
(a) 3.1×109J
(b) −6.3×109J
(c) 6.3×109J
(d) 1.3×1010J