Multiple Choice
If, for an elliptical orbit, rmax = 1025km and e = 0.51, find a, the semimajor axis.
A) 3.25*1024km
B) 6.62 *1025km
C) 6.62 *1024km
D) 5.96 * 1024km
E) 7.28 * 1024km
Correct Answer:

Verified
Correct Answer:
Verified
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