Method and device for generating parameters for satellite orbits and/or satellite clock corrections for a satellite

摘要

The method involves providing a progressive system of differentiable functions with high approximation and a long effective range for describing the satellite orbits and satellite clock corrections. The differentiable functions are transmitted from a function system of parameterized satellite orbits and satellite clock corrections from a ground calculation unit to one or multiple satellites and then transmitted to a user device or from a ground calculation unit without the space segment to a user device. An independent claim is included for a method for generating a parameterization of satellite orbits and satellite clock corrections of satellites.