A satellite is to be placed in a circular orbit so that the centripetal (orbital) acceleration acting on it is 0.30g, where g=9.8m s−2 at Earth’s surface. Estimate the altitude h above Earth’s surface required for this mission. (Take Earth’s radius RE=6.4×106m.) Choose the nearest value.
(a) 1.6×106m
(b) 5.3×106m
(c) 3.2×106m
(d) 1.2×107m