This thesis investigates the challenge of autonomously guiding several satellites into a specific Generic Circular Orbit (GCO) configuration. As the demand for global connectivity and Earth observation scales, traditional ground-based station-keeping becomes computationally prohibitive and operationally inefficient. For this reason, a distributed controller architecture is considered and analysed. The research focuses on the transition from a generic injection point to a specific, stable circular orbit. The dynamics are modelled using the linearised Clohessy-Wiltshire (CW) relative motion equations to represent the state of each satellite relative to a virtual leader or a specific orbital slot. The proposed MPC framework addresses the guidance problem by solving a constrained optimisation problem at each time step.