Unformatted text preview: km 3 /s 2 ) 2. (10 pts) For the same orbit as in Prob. 1, calculate the time at which the satellite will reach = 297 deg. 3. (10 pts) For the same orbit as in Prob. 1, calculate the true anomaly at t = 55000 s. Be sure to state the method used in solving Kepler’s equation....
View Full Document
This note was uploaded on 07/23/2008 for the course AERSP 309 taught by Professor Melton during the Fall '05 term at Penn State.
- Fall '05