A satellite of mass 500kg is launched into a circular orbit at an altitude of 600km above the Earth’s surface. Take Earth’s radius RE=6.4×106m and GME=3.986×1014Nm2/kg.
a. (i) Determine the orbital radius of the satellite measured from the centre of the Earth.
b. (ii) Calculate its orbital speed.
c. (iii) Compute the time period of revolution around the Earth.