M = mass of earth = 5.98 x 1024 kg
a = acceleration due to gravity = 5 m/s2
r = radius of orbit
acceration due to gravity is given as
g = GM/r2
5 = (6.67 x 10-11) (5.98 x 1024) /r2
r = 8.93 x 106 m
orbital period is given as
T2 = 42 r3 /(GM)
T2 = 4 (3.14)2 (8.93 x 106)3 /((6.67 x 10-11) ( 5.98 x 1024))
T = 8391.2 sec
T = 139.85 min
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