If, for an elliptical orbit, r_max = 10²⁵km and e = 0.51, find a, the semimajor axis. A) 3.25*10²⁴km B) 6.62 *10²⁵km C) 6.62 *10²⁴km D) 5.96 * 10²⁴km E) 7.28 * 10²⁴km

Name: If, for an elliptical orbit, r max = 10 25 km and e = 0.51, find a, the semimajor axis. A) 3.25*10 24 km B) 6.62 *10 25 km C) 6.62 *10 24 km D) 5.96 * 10 24 km E) 7.28 * 10 24 km
Brand: Quizplus
Rating: 4.9 (38 reviews)

Question

Quizplus · Accepted Answer

From the given formula: r_max = a(1+e) 10²⁵km = a(1+0.51) a = 6.62 F1F1F1S1F1F1F10 10²⁴km

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

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