with VC arbitrary moment of satellites in orbit Cartesian coordinate systems and Celestial Coordinates of the calculation method different satellites take the initiative to revise its initial state parameters

Packet : 109201254卫星轨道坐标的计算方法.rar filelist
用VC实现对卫星任意时刻在轨道直角坐标系统和天球坐标系中坐标的计算方法.txt

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