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A satellite orbiting Mars has a perigee altitude of 400 km and apogee altitude of 2,000 km. For Mars, use the mean radius of R

A satellite orbiting Mars has a perigee altitude of 400 km and apogee altitude of 2,000 km. For Mars, use the mean radius of R 3,400 km and gravitational parameter of = 4.2828104 km3 /s2

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