= Problem 1: (30 pts) Two radar fixes on an unidentified Earth orbiter yield the following positions: (Assume Earth's ra
Posted: Sun May 15, 2022 11:44 pm
= Problem 1: (30 pts) Two radar fixes on an unidentified Earth orbiter yield the following positions: (Assume Earth's radius is 6378 km) Altitude = 1488 km at a true anomaly ( v ) of 120 deg Altitude = 819 km at a true anomaly ( v ) of 52 deg For this spacecraft's orbit, determine: (a) (5 pts) eccentricity; (b)(5 pts) semi-major axis; (c)(10 pts) altitude of perigee; (d) (10 pts) altitude of apogee.