Description of 2-line elements: http://www.satobs.org/element.html NOSS 3-3 (A) 0.0 0.0 0.0 4.0 v 1 28537U 05004A 05064.39285202 .00000011 00000-0 20000-4 0 01 2 28537 63.4365 85.7823 0128123 179.6051 180.5097 13.39752396 01 Arc 2005 Mar 03.83 - 05.42, WRMS residuals = 0.016 deg NOSS 3-3 (C) 0.0 0.0 0.0 4.0 v 1 28541U 05004C 05064.39294584 .00000011 00000-0 20000-4 0 09 2 28541 63.4331 85.9776 0127620 179.6305 180.4836 13.39772582 00 Arc 2005 Mar 02.79 - 05.42, WRMS residuals = 0.016 deg NOSS 3-3 r 0.0 0.0 0.0 4.7 v 1 28538U 05004B 05064.40221930 .00003510 00000-0 58211-2 0 02 2 28538 63.8270 86.9097 0138295 176.0996 184.1146 13.42833141 04 Arc 2005 Feb 19.20 - Mar 05.43, WRMS residuals = 0.017 deg As of the epoch of 05004C, above, it trailed 05004A by 8.11 s at the ascending node, very nearly their operational separation of 8 s; therefore, at any time, one of them may manoeuvre to match the mean motion of the other, fixing the separation. The Centaur continues its propulsive acceleration, which has reduced its mean altitude by at least 0.8 km since launch, and has reduced it flash period to less than 5 s. Ted Molczan ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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