If, for an elliptical orbit, r_max = 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

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

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

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