A satellite is in a Mars orbit for which the perigee altitude is 350 km and the apogee altitude is 600 km. Find the time interval between periapsis and apoapsis during which the satellite remains below an altitude of 400 km.
A satellite is in a Mars orbit for which the perigee altitude is 350 km and the apogee altitude is 600 km. Find the time interval between periapsis and apoapsis during which the satellite remains below an altitude of 400 km.
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