It is very difficult to achieve effective coverage of hot-spot target in a short time period by earth perturbation for orbital maneuver. because the coverage gap of the temporary multi-satellites network in certain period of time is too large. In this paper. it is assumed that wave beam type of the satellite-payload sensor is a simple conic. https://www.diegojavierfares.com/limited-save-1-64-Lowndes-2010-Triple-Eight-Race-Engineering-Suits-Holden-VE-Commodore-64168-special-save/