An artificial satellite completes one revolution around the Earth in 90min. Take GME=3.986×1014m3s−2 and the Earth’s mean radius RE=6.37×106m.
(i) Convert the orbital period to seconds.
(ii) Calculate the orbital radius of the satellite as measured from the centre of the Earth.
(iii) Determine the height of the satellite above the Earth’s surface.
(iv) Find the linear speed of the satellite in its orbit.