I have just uploaded these three TLEs into the tracking site. The following temporary link can be used: http://www.satflare.com/track.php?q=tempmuos (all the three TLEs will be displayed. Focus is on MECO 1). Best regards, Simone >----Messaggio originale---- >Da: ssl3molcz@rogers.com >Data: 16-feb-2012 15.37 >A: <seesat-l@satobs.org> >Ogg: MUOS 1: pre-launch estimated orbital elements > >MUOS 1 is scheduled for launch today from CCAFS, on an Atlas V-551. The launch window is from 2012 Feb 16 22:46 to 23:30 >UTC. > >Information on the launch is available here: > >http://www.spaceflightnow.com/atlas/av030/status.html > >The following *rough* TLEs are based on launch at window-open. > >MECO 1 167 X 624 km >1 79601U 12047.95718750 .00000000 00000-0 00000-0 0 02 >2 79601 28.0000 308.8000 0337670 130.0000 3.3000 15.58830000 00 > >MECO 2 193 X 34447 km >1 79602U 12047.96724537 .00000000 00000-0 00000-0 0 04 >2 79602 26.0000 311.2000 7227302 179.9293 1.5500 2.38040000 02 > >MECO 3 3463 X 35786 km >1 79603U 12048.07203934 .00000000 00000-0 00000-0 0 01 >2 79603 19.0000 326.7000 6215271 179.0000 74.6500 2.07084000 09 > >Spacecraft separation is planned to occur at T+3:01:23. Soon afterward, the Centaur will conduct a Collision and >Contamination Avoidance Maneuver (CCAM), followed by a blow-down of remaining Centaur propellants. The typical Centaur >end of mission occurs 4400 s after spacecraft separation. > >I have not evaluated visibility windows, but based on a quick look, it appears that the CCAM and blow-down will occur >within range of Western Australia, but well after sunrise. Prospective observers should use the MECO 3 TLE to evaluate >visibility. > >Eventually, the payload will enter an inclined GEO orbit in one of the existing UFO slots. > >Ted Molczan > > >_______________________________________________ >Seesat-l mailing list >http://mailman.satobs.org/mailman/listinfo/seesat-l > _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-l
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