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Title: 卫星位置计算 Download
 Description: After the initial constant is given, the position of the satellite is calculated by iterating the eccentricity anomaly, calculating the angle between ascending node and Greenwich meridian, and the method of calculating satellite velocity is given.
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实验1 0 2017-06-07
实验1\实验一卫星位置计算例程.m 5493 2017-06-18

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