Abstract: The first autonomous non-planar formation flying-around in China was finished successfully by SJ-9A and SJ-9B satellites on November 5, 2012. The collocations and design requirements are introduced. The problems of attitude and orbit coupling and thrust loss are described and analyzed, and the disposals in engineering and numerical simulation results are also given. The results in orbit show that the orbit control time is optimized reasonably and the accuracy of orbit control is guaranteed by amending the orbit control accelerations in uplink via precontrol simulation.