FIELD: space equipment.
SUBSTANCE: invention relates to the rendering of two space objects in a near-circular orbit, for example, a manned spacecraft (MSC) and an international space station (ISS) as a target. MSC is output to a reference orbit having a deviation from the target orbit along the longitude of the ascending node and along the inclination, but with a given discrepancy over the latitude argument. In the vicinity of the line of intersection of the planes of these orbits, an impulse 
combining these planes and simultaneously – the impulse of approach 
, defined by the nominal parameters of the reference orbit. Subsequent approach pulses applied on the second turn are then determined.
EFFECT: technical result of the invention is to shorten the time of approach (up to two turns) of the objects to be rendered (MSC and ISS) with minimal additional costs for approach.
1 cl, 6 dwg
