A communications satellite of mass 650 kg orbits Callira (mass 1.48 x 1023 kg, G = 6.67 x 10-11 N m2/kg2) in a circular orbit of radius r1 = 3.20 x 106 m.
(a)Calculate the orbital speed of the satellite.(3)
(b)Calculate the orbital period of the satellite, giving your answer in hours.(3)
(c)Using E(orbit) = -GMm/(2r), calculate the total orbital energy of the satellite at r1 = 3.20 x 106 m and at a higher orbit r2 = 4.50 x 106 m.(3)
(d)Hence calculate the minimum energy that must be supplied to move the satellite from the orbit at r1 to the orbit at r2.(2)
(Total for Question 3 is 11 marks)