Abstract
Orbit design is a critical aspect of the calibration satellite system, with its effective configuration being integral for successful satellite calibration. This paper addresses the challenge of designing satellite orbits while considering the constraints imposed by satellite-ground equipment performance and launch capabilities. Key factors constraining calibration satellite orbits are analyzed, and orbital constraint equations are developed, focusing on radar performance, calibration time, and regional coverage. The study also introduces a model to assess the efficiency of satellite orbits for calibration purposes, which is rigorously validated through simulation. This study uniquely addresses the integration of radar performance with satellite orbit design, an area not extensively explored in current literature.
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