Multiple Choice
If, for an elliptical orbit, rmin = 1025km and e = 0.86, find a, the semimajor axis.
A) 7.14 * 1024km
B) 7.14 *1025km
C) 13.29 * 1025km
D) 13.29 * 1024km
E) 3.64 *1025km
Correct Answer:

Verified
Correct Answer:
Verified
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