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Perigee describes the point in an orbit closest to earth.
A circular orbit has an apogee exactly twice the altitude of its perigee.
The right ascension of the ascending node is defined from the point where a satellite crosses the prime meridian.
Which parameters define a Keplerian Elements
What eccentricity value does a perfect circle have?
What is/are the orbital element(s) which constantly change throughout a satellite’s orbit?
A satellite designed to take images to monitor the polar ice caps would have an inclination close to what value(deg)?