A satellite moves in a circular orbit of radius r around a planet of mass M.
(a) Obtain an expression for the orbital speed vorb of the satellite in terms of G, M and r.
(b) Derive an expression for the escape speed vesc of a body located at the same distance r from the planet’s centre.
(c) Hence prove that vesc=2vorb.
(d) State the physical significance of the result obtained in part (c).