... 卫星轨道近地点perigee of satellite orbit 卫星轨道根数（又称“卫星轨道参数”）orbit elements of satellite 卫星轨道长半径semi-major axis of satellite orbit ...
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The variation equation of the satellite orbit elements under both J2 and drag perturbations was derived based on the Gauss perturbation equation.
基于高斯摄动方程，推导了卫星在同时考虑J2和大气摄动情况下的轨道根数变化方程。
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