Ballistic Design of Heterogeneous System of the Spacecraft with a Given Cycle of Track Circuit

An approach to the formation of a stable heterogeneous system of the spacecraft is developed. Requirement to provide quasi-synchronous orbits multiplicity is formed. Decomposition of problem of formation of orbits with a given cycle of track circuit is carried out. Method of forming multiple quasi-synchronous orbits of various geometric characteristics of a single cycle of track circuit in the given operating conditions is developed.