Mean Orbital Elements for Geosynchronous Orbit

Astronomy and Astrophysics – Astronomy

Scientific paper

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Scientific paper

The mean orbital elements for geosynchronous satellite are 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 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.

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