The invention provides a ground testing system for the active vibration abatement of a flexible spacecraft, which comprises a marble air-floating platform, a flexible spacecraft motion simulator suspending above the marble air-floating platform, a rate gyroscope, a photoelectric type attitude sensor, a vibration measuring system, an attitude control flywheel, an attitude control thruster, an orbit control thruster, a vibration abatement system, a motion simulator control computer, a ground measurement system and a ground console. The rate gyroscope, the photoelectric type attitude sensor, the vibration measuring system, the attitude control flywheel, the attitude control thruster, the orbit control thruster and the vibration abatement system are mounted on the flexible spacecraft motion simulator. The motion simulator control computer is mounted on the flexible spacecraft motion simulator and is electrically connected with the rate gyroscope, the vibration measuring system, the attitude control flywheel, the attitude control thruster, the orbit control thruster and the vibration abatement system. The ground measurement system is arranged on the marble air-floating platform and the flexible spacecraft motion simulator. The ground console is connected with the photoelectric type attitude sensor, the motion simulator control computer and the ground measurement system. According to the technical scheme of the invention, the defect that the flexible vibration characteristics of flexible spacecrafts are hard to simulate can be overcome. Therefore, the attitude determination accuracy of the flexible spacecraft motion simulator can be improved.