The velocity of a satellite circling around the Earth is computed by the formula...

The velocity of a satellite circling around the Earth is computed by the formula

where M_E = 5.98 X 10²⁴ kg is the mass of the Earth, r the distance from the center of the Earth to the satellite in meters, and G = 6.67 X 10^-11 m³/kg • s² the universal gravitational constant. The unit of the velocity v is m/s. Write a program that inputs the radius r and outputs the satellite’s velocity. Confirm that a satellite that is closer to the Earth travels faster. Define symbolic constants for M_E and G. The distance to the Hubble Space Telescope from the center of the Earth, for example, is approximately 6.98 X 10⁶ m.