David's obs of a second post-manoeuvre pass obviated the need for my search element set, so I have fit it to his and other obs received so far: USA 129 15.0 3.0 0.0 5.3 v 1 24680U 96072A 02255.69324074 .00040447 00000-0 48913-3 0 03 2 24680 97.8836 317.7797 0509903 194.9552 359.5098 14.78629276 06 WRMS error = 0.01 deg Only the B* decay element was held constant in the analysis. The epoch is near the time of the manoeuvre, which occurred when the object was near perigee, near 14 S, 105 W. I hope to obtain a few more points this evening. Ted Molczan ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www.satellite.eu.org/seesat/seesatindex.html
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