FIELD: space apparatus engineering. SUBSTANCE: method includes one ore more artificial satellites launching into ring multiple synchronous orbit of nought inclination determining by formula where m and n are numbers of draconic periods of satellite orbital revolution and effective periods of earth rotation during repetition period of satellite trace (taking into account nods line regression). Numbers remainder is choosing odd and earth surface image is working out during time less then period of satellite trace repetition in swath belt angle equal to 180 deg divided by number m. EFFECT: better quality of visual information for setting up number of satellites. 8 dwg
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Authors
Dates
1997-03-27—Published
1988-09-09—Filed