3: Elliptical orbit (10 pts.) 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. A. For the elliptical transfer orbit, find the following quantities: 1. The semi-major axis 2. The distance from the center of the orbit to the satellite, . (Hint: First label on the diagram the location of the 2 foci of the ellipse, the distance , and the distance . Then find .) 3. The eccentricity