Find the altitude of a satellite in a circular orbit around earth with a velocity of 7000 m/s.
Find the altitude of a satellite in a circular orbit around earth with a velocity of 7000 m/s. Correct Answer 1751.6 km
From the relation us = Ro√(go/Ro+h), using us = 7000 m/s, Ro = 6374 x 103 m, we have h = – Ro h = 1751.6 km.
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Feb 20, 2025