FIELD: communication.
SUBSTANCE: invention relates to communication engineering and can be used in satellite communication systems. For this purpose, method of controlling satellites provides a service using a given moment in time to at least one portion of a set of said satellites, in which, continuously or pseudo-continuously, a mean value of longitudes of respective ascending nodes of each satellite is computed, and, for each satellite, a correction of trajectory of satellite is applied by regulating longitude of ascending node on a setpoint equal to said current mean value.
EFFECT: technical result consists in improved carrying capacity.
7 cl, 3 dwg
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