LET KINETIC ENERGY OF A SATELLITE IS X,THEN ITS TIME OF REVOLUTION T IS PROPORTIONAL TO

Dear Student,

We have,

12mv2=x  or v2=2xm...(i)Now, mv2R=GMmR2   ( for a satellite )or v2=GMR..(ii)from (i) and (ii)GMR=2xmor R=GMm2x..(iii)Now Time Period:  T=Perimeter of Circlevelocity2πRv  ( Assuming its a circular orbit)using (i) and (iii)T=2π×GMm2x×m2xor, T=πGM2m321x3   Note: The bracket term is a constantor, T=const×1x3Or, T1x3   Tx-32
Regards.

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