If, for an elliptical orbit, r_min = 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

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The Answer of If, for an elliptical orbit, r_min = 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

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

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