The shape and perigee of artificial satellite orbits shall continually variate due to caused by the atmospherical drag and the earth gravity.
人造地球卫星的轨道由于大气阻力和地球引力场等因素的摄动,其形状和近地点位置将不断改变。
This paper deals with the characteristic, the USES and the calculation of orbits of earth synchronous satellite.
本文阐述了地球同步卫星的特征、用途及其轨道计算。
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。
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