Planet A's satellite has an elliptical orbit described by X2 2 + v =1. (509132 (4?52)2 (All units are in miles.) The coordinates of the center of PlanetA are (25,0). Complete parts a and b below. a. The perigee of the satellite's orbit is the point that is nearest PlanetA's center. It the radius of PlanetA is approximately 3955 miles. nd the distance at the pen'gee above PlanetA's surlace. The perigee's distance above Planet A's surface is miles. b. The apogee of the satellites orbit is the point that is the greatest distance from Planet A's center. Find the distance of the apogee above PlanetA's surface. The apogee's distance above Planet A's surface is miles.