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 Sofa Chaise 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 Mini Fridge geostationary satellite from this mean orbit position is less than 1800m.The mean elements of ec and es are obtained.
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