Two communication satellites A and B revolve around the Earth in separate circular orbits. Satellite A takes 6h to complete one revolution, while satellite B takes 12h.
(i) Derive the general relation between their orbital radii rA and rB in terms of their respective periods TA and TB.
(ii) Using the relation obtained, find the numerical ratio rArB.
(iii) Taking the Earth’s radius as 6.37×106m, calculate the difference in heights of the two satellites above the Earth’s surface.