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 ------------------------------------------------------------------------ 080/02:40:34.719 0.0 0.6 0.6 N/A -0.5 -0.0 186.6 000/00:05:09.439 0.3 -0.1 180.6 TWO LINE MEAN ELEMENT SET Precicted orbit before orbit raising ISS 1 25544U 98067A 08079.40333919 .00020000 00000-0 20000-3 0 9027 2 25544 51.6384 119.2279 0001183 271.9495 88.1534 15.76341091 14360 Predicted orbit after orbit raising ISS 1 25544U 98067A 08080.16407427 .00020000 00000-0 20000-3 0 9039 2 25544 51.6347 115.3043 0000915 317.1792 42.9301 15.76244056 14486 Looking for the perfect gift? Give the gift of Flickr! http://www.flickr.com/gift/ ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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