Ted posted: >I have fit the following approximate elements, derived from the integrated >elements: > >1 70000U 09083.04470105 .00003428 00000-0 53540-3 0 08 >2 70000 27.3299 131.9871 6846226 267.5576 19.1640 2.85634715 05 My guess is: 1 90061U 06667A 09083.04414421 .00002770 00000-0 44300-3 0 04 2 90061 27.3291 132.1183 6847812 267.3920 18.7125 2.85353204 02 Ted posted: >I suspect that the mean motion could be off by at least 0.01 rev/d, which would >result in a prediction time uncertainty of at least 5 min after one day. I hope that the mean motion may be off only about 0.005 revs/day. This would be about 3 minutes/day uncertainty. Mike McCants ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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