http://spaceflight1.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/orbit/ISS/SVPOST.html Maneuvers contained within the current ephemeris are as follows: IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP ------------------------------------------------------------------------ 293/19:22:12.506 1.2 1.9 1.9 N/A -1.4 -0.0 195.5 000/00:04:21.013 0.2 0.1 185.1 TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 10293.50387128 .00016717 00000-0 10270-3 0 9051 2 25544 51.6446 309.4339 0007585 113.5581 246.6378 15.72173351 3181 ISS 1 25544U 98067A 10293.82169646 .00016717 00000-0 10270-3 0 9060 2 25544 51.6453 307.8062 0005787 116.8339 243.3416 15.71792133 3230 _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-l
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