The invention relates to the technical field of integrated spaceflight devices, in particular to a plate frame type satellite device suitable for a high earth orbit satellite. The plate frame type satellite device comprises an electronic cabin top plate, an electronic cabin front plate, an electronic cabin rear plate, electronic cabin side plates, an electronic cabin partition plate, a main force-bearing front plate, a main force-bearing rear plate, main force-bearing side plates, a bottom plate, a transition sleeve and a cushion plate. According to the plate frame type satellite device, a central force-bearing barrel is omitted, a plate frame is used as the main force-bearing structure, and uniform transition of whole satellite mechanical loads from a box type plate frame platform to a round carrying butt-joint ring is achieved; the plate frame type satellite device has the characteristics of being simple, flexible, high in expandability and suitable for an electric propulsion satellite platform; the satellite space utilization efficiency is effectively improved, and the effective load bearing capacity is improved.