GongDimian

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文件大小:9KB
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上传日期:2020-02-25 16:50:14
上 传 者Vastace
说明:  本文件为STK Senario。演示了一类共地面轨迹的卫星星座,演示时长为2天。卫星轨道的半长轴a=10541km,偏心率e=0,轨道倾角i=63.4°,近地点幅角0度,右旋升交点赤经 =27.7398°,真近点角 =330°。轨道整体为M=1,N=8的回归轨道,符合共地面轨迹星座的要求。
(This document is STK senario. A kind of satellite constellation with common ground orbit is demonstrated. The demonstration time is 2 days. The semi major axis of the satellite orbit is 10541km, the eccentricity is e = 0, the orbit inclination is I = 63.4 degree, the perigee angle is 0 degree, the right ascension intersection right ascension right longitude is 27.7398 degree, and the true perigee angle is 330 degree. The overall orbit is a regression orbit of M = 1, n = 8, which meets the requirements of common ground orbit constellation.)

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GongDimian.sc, 72605 , 2020-02-25

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