Xiaoya Wang
Abstract
Evolution features are presented for several key orbit elements,based on simulations of inclined geosynchronous satellite via STK software.It is found out that inclined geosynchronous orbit is stable.Such kind of orbits can meet the stability requirement for navigation satellites.
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Evolution features are presented for several key orbit elements,based on simulations of inclined geosynchronous satellite via STK software.It is found out that inclined geosynchronous orbit is stable.Such kind of orbits can meet the stability requirement for navigation satellites.
Key concepts: Geosynchronous orbit, Orbit (dynamics), Satellite, Aerospace engineering, Geodesy, Remote sensing, Software, Medium Earth orbit