System for adjusting the position and attitude of orbiting bodies using guide satellites that includes a satellite (1) fitted with a system for outputting a high-speed ion stream (3) and a secondary propulsion system (4), said satellite being located close to a body (2) the orbit and/or position of which is to be adjusted, and the position of the satellite being controlled such that the ion stream generated is directed against the body (2) generating the thrust necessary to adjust the orbit and/or orientation thereof. The system can be used to move active satellites, space debris or any other celestial body, transmitting the necessary thrust without physical contact with the body the orbit and/or orientation of which is to be adjusted. This helps to prevent problems related to collisions in orbit and enables complex rendezvous and docking manoeuvres.