The paper defines the concept of the structure self-stabilization for satellite constellation,and analyzes the configuration stability of satellite constellation influenced by the main perturbations.Then the method is designed to realize the structure self-stabilization for satellite constellation through changing the deviations of the semi-axis and the inclination.Finally the design of the structure self-stabilization for an example constellation has carried,and the design results indicate that the design of the structure self-stabilization for satellite constellation has enhanced the configuration stability for satellite constellation.