https://spaceflight.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 ------------------------------------------------------------------------ 270/16:51:48.829 -0.9 1.4 1.4 N/A -0.9 0.0 220.7 000/00:03:37.658 -0.6 0.0 215.8 TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 17269.95286634 .00016717 00000-0 10270-3 0 9151 2 25544 51.6387 251.0122 0004395 325.2303 34.8562 15.54238236 37573 ISS 1 25544U 98067A 17270.72442880 .00016717 00000-0 10270-3 0 9166 2 25544 51.6415 247.1674 0004505 316.9808 43.0992 15.54017485 37696 _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-lReceived on Thu Sep 14 2017 - 20:05:48 UTC
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