At time t0 (relative to perigee passage), the position r and velocity v of a satellite in the ge

Question

Cyra Jelle Calleja · Accepted Answer

1. First, we need to find the orbital elements of the satellite at time t0. We can use the follo

At time t0 (relative to perigee passage), the position r and velocity v of a satellite in the geocentric equatorial frame are r = {-5000 , -8000, -2100} km v = {-4 , 3.5, -3} km/s Find r and v at t1 = t0 + 60 min.