In order to achieve high resolution optics remote sensing of the Geostationary Orbit (GEO), the difference of dynamics conditions between the low orbit and GEO has been researched. The problem about volume of camera enlarged by the long time of powered phase, disadvantageous dynamics conditions, frame mapping and long distance has been analyzed. The simulation camera of GEO Resolution 21.5 m has been researched, and then the dynamics conditions test has been taken and the testing parameters of camera key position have been obtained. It is proved that research of payload which is the key part of the high resolution optics remote sensing of GEO is feasible.