In a few hours, they will raise the iss orbit, using the ATV. 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 ------------------------------------------------------------------------ 171/06:51:03.282 8.8 11.2 11.2 N/A -3.7 0.1 187.1 000/00:20:06.565 -5.7 0.1 186.9 TWO LINE MEAN ELEMENT SET Predicted orbit before orbit raising ISS 1 25544U 98067A 08170.54809449 .00020000 00000-0 20000-3 0 9008 2 25544 51.6390 9.3694 0006297 342.2051 17.8893 15.77011640 28747 Predicted orbit after orbit raising ISS 1 25544U 98067A 08171.30851600 .00020000 00000-0 20000-3 0 9010 2 25544 51.6412 5.4486 0008790 269.0804 90.9352 15.74596586 28869 Kevin __________________________________________________________________ Yahoo! Canada Toolbar: Search from anywhere on the web, and bookmark your favourite sites. Download it now at http://ca.toolbar.yahoo.com. ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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