Ted posted: >Int2 propagates it to the following elements today: > >1 90011U 02624A 10252.65005378 .00000067 00000-0 00000-0 0 05 >2 90011 27.0033 212.1385 7276652 352.1241 0.8539 2.00729668 08 The observations of this object near apogee were from Austria. I have fit the observations to three possible orbits: 1 90011U 02624A 10252.89820192 .00000000 00000-0 00000+0 0 06 2 90011 27.6839 208.6061 7232950 355.8376 350.2684 2.00200000 08 1 90011U 02624A 10252.89820192 .00000000 00000-0 00000+0 0 06 2 90011 27.6849 208.6147 7237984 355.7832 351.5482 2.00600000 06 1 90011U 02624A 10252.89820192 .00000000 00000-0 00000+0 0 06 2 90011 27.6859 208.6233 7243009 355.7290 352.8278 2.01000000 08 The mean motion is somewhat uncertain. I hope that the correct mean motion will be between 2.002 and 2.010. Mike McCants _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-l
This archive was generated by hypermail 2b29 : Fri Sep 10 2010 - 05:42:46 UTC