Determine the perigee altitude of the elliptical orbit so that Satellites A and B occupy the same radial position when Satellite A firstly arrives the apogee point (in other words, Satellites A and B perform a rendezvous maneuver at apogee of satellite B).
Determine the perigee altitude of the elliptical orbit so that Satellites A and B occupy the same radial position when Satellite A firstly arrives the apogee point (in other words, Satellites A and B perform a rendezvous maneuver at apogee of satellite B).
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Determine the perigee altitude of the elliptical orbit so that Satellites A and B occupy the same radial position when Satellite A firstly arrives the apogee point (in other words, Satellites A and B perform a rendezvous maneuver at apogee of satellite B).
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