Integrated ultra-low orbit constellation carrying platform

An integrated ultra-low orbit constellation carrying platform comprises an air inlet cabin section, a middle cabin section and a tail cabin section, an air inlet channel is arranged in the air inlet cabin section, a radio frequency ionization chamber, an electric control solid propeller storage cabin and a satellite storage cabin are arranged in the middle cabin section, and a magnetic spraying accelerating tube, a propellant supplementing mechanism and an electric control solid rocket upper stage are arranged in the tail cabin section. The air inlet channel, the radio frequency ionization chamber and the magnetic spraying accelerating pipe are communicated to form a carrying platform air suction type electric propulsion system. The satellites are connected with the upper stages of the corresponding electronic control solid rockets in the launching channels. In the satellite transportation orbit injection networking stage, the upper stage of the electronic control solid rocket carrying the satellite goes out