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.roneverhart.com/HP-Notebook-15-da0008ca-HD-LED-15-6-Touchscreen-Intel-Core-i5-8250U-1-6-GHz-8-GB-RAM-1-TB-SSD-HDMI-USB-Multi-format-S/