A satellite of mass m moves in a circular orbit around a planet of mass M.
(a) Using an appropriate physical argument, derive an expression for the satellite’s orbital speed v in terms of G, M, and the orbital radius r.
(b) Express the orbital period T in terms of r, M, and G.
(c) Eliminate r to write the satellite’s total mechanical energy E exclusively in terms of m, M, G, and T. Show each algebraic step clearly.
(d) A 250kg satellite has an orbital period of 90.0min around Earth. Using your expression from part (c), calculate its total mechanical energy.