Question: The speed in miles per hour of a satellite moving in a circular orbit about a celestial body is given approximately by
Speed = √(C/D)
where C is a constant depending on the celestial body and D is the distance from the center of the celestial body to the satellite (in miles). Write a program that reads the value of the constant C for a celestial body and a value for D and then displays the speed of the satellite. Run the program with the following values: (earth) C = 1 .2E12, (moon) C = 1 .5ElO, (Mars) C = 1 .3E 11.