Particularly, the method of coverage orbit design is given in view of the orbital period deviation, which is based on recursive orbit.

特别是，以循环轨道为基础，考虑轨道周期的误差，给出覆盖轨道的设计方法。

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In this paper, a series of characters for recursive orbit and coverage orbit of satellites are discussed, and the method of recursive orbit design is given.

本文阐述人造卫星循环轨道与覆盖轨道的一系列性质，给出确定循环轨道的方法。

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