The satellite orbits the earth in its regular orbit.
卫星在它的固定轨道里绕地球飞行。
This paper presents a new method to classify satellite orbits and the basic Characterization of stay orbit.
本文给出卫星轨道分类的一个新方法和逗留轨道的基本特性,这一特性可用于卫星轨道的初步设计。
The GPS ephemeris and GLONASS ephemeris adapt to some kind of the satellite orbits while they have some shortcoming.
GPS和GLONASS广播星历形式适合于某一类卫星轨道,但存在一定局限性。
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