1. The problem statement, all variables and given/known data 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? 2. Relevant equations Velocity = square root (G * m/r) 3. 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!!!!!