A research satellite of negligible mass is placed in a circular orbit at an altitude of 300km above Earth’s surface. The radius of Earth is 6.37×106m and Earth’s mass is 5.97×1024kg. The universal gravitational constant is G=6.67×10−11Nm2kg−2.
(1) Calculate the speed of the satellite in its orbit, expressing your answer to three significant figures with appropriate units.
(2) Determine the orbital period of the satellite. Express your answer in minutes.
(3) Compute the ratio ∣Ug∣K of the satellite’s kinetic energy K to the magnitude of its gravitational potential energy Ug while in orbit, and interpret the physical meaning of the value you obtain.
(4) Qualitatively describe how the orbital speed would change if the satellite were instead placed in a circular orbit at an altitude of 600km above Earth’s surface, citing relevant physical relationships in your explanation.