A satellite in sunsynchronous polar orbit has a tangential (orbital) speed of 7.85 X 10^{3} m s^{-1}. The mass of the earth is M_{earth }= 5.98x10^{24} kg, the gravitational constant is G = 6.67 x 10^{-11} N
m^{2}/kg^{2 }and the radius of the earth is R_{earth} = 6.37 x 10^{6} m. Remember that the orbital radius, R = R_{earth} + h. [Hint: Mathematics of Satellite Motion Review Sheet.] What is the height (h) of the satellite's orbit?