equatorial orbit

基本解釋

All geostationary satellites orbit the earth in the equatorial plane at a height of 35,785 km above the equator and stand still at a fixed azimuth and altitude for an observer on the earth surface.
所有的地球同步衛(wèi)星都在赤道上空35，785 km高度運行，相對于地面觀測者來說，它們的方位角和高度角是始終不變的。
Lagranges method is employed to derive the equations of motion for the system when the satellite is restricted to an orbit plane(such as the equatorial plane) and moves at a uniform angular velocity.
利用拉格朗日方法導(dǎo)出母星被限制在赤道面上以均勻角速度運動時系統(tǒng)的動力學(xué)方程。