The orbit variation in one day under the nonspherical perturbation is shown and the motion of the orbit plane is computed.
计算给出了一日内的卫星轨道，反映了在地球非球形摄动下轨道的变化情况，且对轨道面的进动进行了计算。
For two cases of the receiver in and out of the orbit plane, the path gain of TE and TM wave is discussed in the procedure of simulation, respectively.
在仿真过程中，假设了接收机在卫星轨道面内和轨道面外两种情况，分别对TE波和TM波的路径增益进行了讨论。
For two cases of the receiver in and out of the orbit plane, the path gain of TE and TM wave is discussed in the procedure of simulation, respectively.
在仿真过程中，假设了接收机在卫星轨道面内和轨道面外两种情况，分别对TE波和TM波的路径增益进行了讨论。
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