you are in charge of placing a satellite of mass 5130kg into an orbit around the planet Jupiter. The orbit has an altitude of 3.59E+5m.
What is the orbital velocity of the satellite?
Velocity = square root (G * m/r)
The Attempt at a Solution
Velocity = square root (6.67e-11 * 5130/3.59e+5)
V = 9.76e-7 which is Incorrect.
Any Help would be much appreciated!!!!!