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.
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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