A satellite in sunsynchronous polar orbit has a tangential (orbital) speed of 7.85 X 103 m s-1. The mass of the earth is Mearth = 5.98x1024 kg, the gravitational constant is G = 6.67 x 10-11 N m2/kg2 and the radius of the earth is Rearth = 6.37 x 106 m. Remember that the orbital radius, R = Rearth + h. [Hint: Mathematics of Satellite Motion Review Sheet.] What is the height (h) of the satellite's orbit?