A transfer orbit is an elliptical orbit meant to move satellites between two different-radius circular orbits. A satellite with mass = 3000 kg is in a circular orbit with 1 = 20,000 km. It needs to be moved into lager orbit with r2 = 25200km. The satellite is moved from orbit 1 into the transfer orbit at point A, and then is moved into orbit 2 at point B. How much energy was added to get the satellite from orbit 1 into the transfer orbit