Here is a very preliminary orbit that is a good fit to David Brierley's recovery observation: USA 89 r 4.0 2.0 0.0 5.5 v 1 22519U 92086 C 99308.19880139 .00004000 00000-0 63097-3 0 07 2 22519 56.9390 337.5498 3379000 328.1344 159.3986 8.47437568 02 To produce these elements, I began with elements from epoch 99205, and adjusted the decay rate to produce a close fit to David's observations. Using this decay rate as a mean value, I propagated the mean motion to an epoch coincident with the time of the observations, and precessed the RAAN and argument of perigee accordingly. Finally, I set the decay rate a nominal value that I believe should be close to reality. I expect prediction accuracy to be well within about 1 minute of time after 1 day. I will be able to produce a much more reliable orbit after additional observations are made. Ted Molczan ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www2.satellite.eu.org/seesat/seesatindex.html