The orbital reconfiguring problem after maneuver failure for rendezvous phasing is studied. The orbital reconfiguring design rules are proposed and four types of orbital reconfiguring plan are provided respectively for every maneuver failure in five-impulse phasing mission. Based on the proposed design rules, the provided reconfiguring plan's correcting ability, tracking and command condition, propellant consumed, terminal precision and security are analyzed. Finally, the orbital counter plan to deal with rendezvous phasing maneuver failure is obtained.