This paper introduces methods of calculation the initial orbit of the satellite only with the velocity vectors of two epochs.
本文介绍了仅用卫星两个时刻速度向量计算卫星初轨的方法。
This paper introduces methods of calculation the initial orbit of the satellite only with the velocity vectors of two epochs.
本文介绍了仅用卫星两个时刻速度向量计算卫星初轨的方法。
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