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Assume that you wish to
place in orbit a satellite that
always remains directly
above the same point on
the Earth's equator. What
velocity and altitude must
the satellite have at the
instant of burnout of the
rocket booster?
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Transcribed Image Text:Assume that you wish to place in orbit a satellite that always remains directly above the same point on the Earth's equator. What velocity and altitude must the satellite have at the instant of burnout of the rocket booster?
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