1. Armellin, R., San-Juan, J.F., Lara, M.: End-of-life disposal of high elliptical orbit missions: the case of INTEGRAL. In: Advances in Space Research. Advances in Asteroid and Space Debris Science and Technology—Part 1, vol. 56(3), pp. 479–493 (2015). doi:
10.1016/j.asr.2015.03.020
2. Breakwell, J.V., Vagners, J.: On error bounds and initialization in satellite orbit theories. Celest. Mech. 2, 253–264 (1970). doi:
10.1007/BF01229499
3. Chapront, J., Francou, G.: The lunar theory ELP revisited. Introduction of new planetary perturbations. Astron. Astrophys. 404, 735–742 (2003). doi:
10.1051/0004-6361:20030529
4. Chapront-Touze, M., Chapront, J.: ELP 2000–85—a semi-analytical lunar ephemeris adequate for historical times. Astron. Astrophys. 190, 342–352 (1988)
5. Coffey, S.L., Neal, H.L., Segerman, A.M., Travisano, J.J.: An analytic orbit propagation program for satellite catalog maintenance. In: Alfriend, K.T., Ross, I.M., Misra, A.K., Peters, C.F. (eds.) AAS/AIAA Astrodynamics Conference 1995, Advances in the Astronautical Sciences, vol. 90, pp. 1869–1892. American Astronautical Society, Univelt Inc, USA (1996)