Using Alan's SatAna/SatEvo with (more or less) standard parameters: DELTA 2 R/B 183 x 134 km 1 28377U 04026B 04267.11929492 .13823163 11136+0 27470-3 0 91548 2 28377 102.9962 264.4125 0037332 81.8896 278.5338 16.42682081 10926 DELTA 2 R/B 176 x 131 km 1 28377U 04026B 04267.18016785 .16140905 14609+0 25904-3 0 91544 2 28377 102.9956 264.5377 0034489 81.6815 278.7095 16.44500040 10937 DELTA 2 R/B 169 x 128 km 1 28377U 04026B 04267.24096672 .19641628 23820+0 24630-3 0 91545 2 28377 102.9949 264.6632 0031111 81.4731 278.8794 16.46657872 10944 DELTA 2 R/B 159 x 124 km 1 28377U 04026B 04267.30167508 .25847011 45451+0 23941-3 0 91548 2 28377 102.9940 264.7888 0026892 81.2643 279.0402 16.49377588 10955 DELTA 2 R/B 144 x 117 km 1 28377U 04026B 04267.36226210 .41351800 13714+1 25086-3 0 91544 2 28377 102.9929 264.9148 0021026 81.0550 279.1830 16.53271845 10963 Final decay at 4267.423464 (Sept.23 10:10 113E, 12S, perigee around 10:25 90E, 50N) ----Ursprungligt meddelande---- This object with the interesting inclination of 103 degrees, being the rocket from the Aura launch, appears likely to decay early on 23 September UTC. It has an RCS value of 11.00 so could provide an interesting observation if decay is seen. ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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