Truncation of the geopotential model for the determination of satellite orbits with small excentricities.

Physics

Scientific paper

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Geopotential: Models, Artificial Satellites: Orbit Determination

Scientific paper

The upper bounds of the perturbation of satellite orbits with small excentricities due to spherical harmonics of the geopotential are estimated using an analytical solution derived by the author. In a further step a method is developed to define the truncation limit of the geopotential model for orbit determinations. The truncated model suggested for the GPS-orbit determination differs slightly from an 8x8-model by the consideration of the resonance character of the GPS-orbits.

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