Mean Orbital Elements for Geosynchronous Orbit - I - Semi-major, eccentricity, and longitude of perigee

Mean Orbital Elements for Geosynchronous Orbit - I - Semi-major, eccentricity, and longitude of perigee

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The mean orbital elements for geosynchronous satellite are Head torches developed in terms of non-singular orbital elements.The true satellite position oscillates about the position calculated from the mean elements due to short period Riso Print perturbations to the satellite motion.the displacement of a geostationary satellite from this mean orbit position is less than 1800m.

The mean elements of ec and es are obtained.