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A satellite is in a circular orbit with a radius of 6570 km and an inclination of 28º.
It needs to be moved to a circular orbit with a radius of 42,160 km and an inclina-
tion of 0°. This scenario could be a satellite launched from Cape Canaveral in
Florida headed for a geostationary orbit.
Find the total burn using the most fuel-efficient transfer.

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