In a satellite if the time of revolution is T, then K.E. is proportional to
1T
1T2
1T3
T−2/3
v=GMr ∴K.E.∝v2∝1r---(1) and T2∝r3⇒T23∝r⇒1r∝T-23---(2) From (1) and (2) we get ∴ K.E. ∝T−2/3