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