FIELD: astronautics.
SUBSTANCE: invention relates to spacecraft (SC) on-board equipment. Method includes determination of atmospheric density at altitude of SC orbit, position of center of mass and SC orientation, prediction of boundaries of location area of observation object relative to SC orbit, generation of commands for control of observation equipment (OE). At the preset observation interval, the most suitable SC window is determined. Said movable mirror (MM) is arranged on SC to provide visibility of OE through window, MM and stationary mirror placed on SC, certain points in location area of observation object. Shooting is performed during MM reorientation entire time.
EFFECT: technical result consists in providing guaranteed recording of data from an observation object of a different removable OE using the described system of mirrors.
1 cl, 1 dwg
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