The velocity of the satellite revolving round the Earth at a height r from the centre of the Earth is given by
v=(rGM)...(1)
The formula to calculate the time period in the circular orbit is given by
T=v2πr...(2)
In this case: r=R+R=2R
Substitute the expression for the velocity from equation (1) into equation (2) and simplify to obtain the required time period.
T=====rGM2πr2gR2π×2RπR4πR242R32R