Space debris is posing a serious threat to human space activities and is needed to be measured and cataloged. With the development of space exploration technology, the measurement accuracy of debris is constantly improved, the measurement station is constantly increasing, and the accuracy of orbit determination and prediction of space debris is needed. By using the precise ephemeris of TerraSAR-X, we simulated photoelectric measurements of space debris, and evaluated effect of the empirical forces compensation model on the orbit and the prediction accuracy of space debris based on the same multi-stations’ simulation data of right ascension and declination. According to the orbital determination results by simulation data of right ascension and declination, the accuracy of about 50% data arcs increased about 25%.