The satellite split off from the rocket about 25 minutes after its 00:20 lift-off, entering a geosynchronous transferorbit.
“鑫诺二号”卫星于29日零时20分点火升空，25分钟后与运载火箭分离，进入地球同步转移轨道。
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A fast design method for transferorbit of lunar probe is presented using overlap conic curve method aimed at lunar landing transferorbit and lunar satellite transferorbit.
The propulsion subsystem is essential for maneuvering the MUOS satellite during transferorbit to its final location as well as conducting on-orbit repositioning maneuvers throughout its mission life.