A spacecraft is in an orbit with a perigee height of 280 km, an apogee height of 400 km, and an inclination of 51.33⁰. Find the rates of the node regression and perigee advance.

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1

A spacecraft is in an orbit with a
perigee height of 280 km, an
apogee height of 400 km, and an
inclination of 51.33⁰. Find the rates
of the node regression and
perigee advance.
Transcribed Image Text:A spacecraft is in an orbit with a perigee height of 280 km, an apogee height of 400 km, and an inclination of 51.33⁰. Find the rates of the node regression and perigee advance.
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