Orbit Design for Approaching Multiple Space Objects in a Circular Orbit

This paper focuses on orbit design for a spacecraft without orbital maneuver approaching multiple objects in a circular orbit. Based on the assumption of no perturbation, a series of relations of approach orbit elements and geocentric angle between objects are established by theory analysis and formula derivation. Then characteristics of approach orbit are derived from a large number of data and numerical analysis. Finally a simulation example with Earth Geostationary Orbit as target circular is shown.