Multiple Choice
If, for an elliptical orbit, rmax = 1025km and e = 0.79, find a, the semi-major axis.
A) 1.17 *1025km
B) 4.76 *1025km
C) 5.59 * 1025km
D) 5.59 * 1024km
E) 1.17 * 1024km
Correct Answer:

Verified
Correct Answer:
Verified
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