Resumen: The aim of the time distribution methodology presented in this paper is to generate constellations whose satellites share a set of relative trajectories in a given time, and maintain that property over time without orbit corrections. The model takes into account a series of orbital perturbations such as the gravitational potential of the Earth, the atmospheric drag, the Sun and the Moon as disturbing third bodies and the solar radiation pressure. These perturbations are included in the design process of the constellation. Moreover, the whole methodology allows to design constellations with multiple relative trajectories that can be distributed in a minimum number of inertial orbits. Idioma: Inglés DOI: 10.1007/s10569-016-9747-3 Año: 2017 Publicado en: Celestial Mechanics and Dynamical Astronomy 128 (2017), 197-219 ISSN: 0923-2958 Factor impacto JCR: 2.121 (2017) Categ. JCR: MATHEMATICS, INTERDISCIPLINARY APPLICATIONS rank: 30 / 103 = 0.291 (2017) - Q2 - T1 Categ. JCR: ASTRONOMY & ASTROPHYSICS rank: 34 / 65 = 0.523 (2017) - Q3 - T2 Factor impacto SCIMAGO: 1.092 - Applied Mathematics (Q1) - Computational Mathematics (Q1) - Modeling and Simulation (Q1) - Mathematical Physics (Q1) - Space and Planetary Science (Q2) - Astronomy and Astrophysics (Q2)