The payload should have a 717 minute period: NROL-1 1 99991U 04245.01643588 0.00000000 00000-0 00000-0 0 00 2 99991 59.2900 231.1000 7450000 304.8700 356.1300 2.00500000 04 But it should maneuver to a 63 degree inclination. The Centaur may be in a lower orbit, but the mean motion is very uncertain: NROL-1 Centaur 1 99992U 04245.01789074 0.00000000 00000-0 00000-0 0 02 2 99992 59.2900 231.1000 7450000 303.8700 357.1300 2.05000000 05 These elsets fit Ted's observations. Mike McCants ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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