The space rendezvous and remote-guided mission planning methold of the orbital maneuver is researched in this thesis. The matter is resolved by translating double impulse problem into gaussian problem. the initial position and the flighting time is ergodic caculated by Battin-Vaughan algorithm. The three-dimensional surface map and contour map of the maneuver time, the tracker initial true anomaly and the required characteristic velocity is made in this thesis. The mission of spacecraft rendezvous and intercept in space is planned. Simulation results show that the using of Battin-Vaughan for solving the Gaussian question is effective. Such as space rendezvous and interception mission analysis, the mapping and analysis of the contour map as a mission planning support tool can intuitively and quickly provide a reference for engineering applications.