FIELD: space engineering.
SUBSTANCE: proposed system can be used for space optical communications between objects, such as man-made Earth satellites, space vehicles, and orbital stations. It has airborne transceiving equipment complex that functions to evaluate parameters of space object trajectory in the course of its flight which makes it possible to qualify predicted values of mentioned parameters within any desired moment of time dispensing with means other than those incorporated in transceiving equipment complex.
EFFECT: facilitated in-flight evaluation of desired parameters of space object trajectory and orientation.
1 cl, 1 dwg
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