The results can be used as approximate values of the initial satellite orbit to correct the orbit by integration or calculate satellite ephemerides.
计算结果均可以做为轨道改进和计算星历时的人卫初轨近似值。
The results can be used as approximate values of the initial satellite orbit to correct the orbit by integration or calculate satellite ephemerides.
计算结果均可以做为轨道改进和计算星历时的人卫初轨近似值。
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