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

The mean orbital elements for geosynchronous satellite are Bicycle Computers 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 Steamrollers is less than 1800m.The mean elements of ec and es are obtained.