Satellite orbit determination method in single station

摘要

PURPOSE: A satellite orbit determination method in a single station is provided to implement position determination of a satellite in real time and establish an operation orbit system for a geostationary satellite. CONSTITUTION: A satellite orbit is predicted based on station observation data which are received in real time automatically through ranging and angle tracking of a single station and accumulated for a specified period of time(S605). Simulation observation data about the outside observation site is created based on the information of the predicted satellite orbit and the location information of a selected outside observation site. An azimuth bias is predicted using the accumulated station observation data and the simulation observation data.