If, for an Elliptical Orbit, R_min = 10²⁵km and E

Multiple Choice

If, for an elliptical orbit, r_min = 10²⁵km and e = 0.55, find a, the semimajor axis.

A) 2.44*10²⁵km
B) 2.22 * 10²⁵km
C) 2.44 * 10²⁴km
D) 2.22 * 10²⁴km
E) 1.72 *10²⁵km