Your prediction software, like VEC2TLE that I used to produce these elsets, may treat the missing zero before 3353. incorrectly. USA 129 +19 m/s 1 24680U 96072A 03353.75010000 .00027406 00000-0 28356-3 0 11 2 24680 97.7982 53.4604 0545501 117.4163 359.3733 14.72878899 207 ... > You can make search elsets by just adding > small +- increments to MM, eg 14.719 14.739 and 14.733 14.753 ... Since we don't know the time of manoeuvre, and my Epochs are close to the expected time, there is little reason to change other elements. Of course if MM is way off, the apogee height (ie eccentricity) needs adjustments, so for these cases better use Ted's full set of elsets. > > USA 129 +19 m/s > 1 24680U 96072A 3353.75010000 .00027406 00000-0 28356-3 0 11 > 2 24680 97.7982 53.4604 0545501 117.4163 359.3733 14.72878899 207 > USA 161 +14 m/s > 1 26934U 01044A 03353.84324512 .00002200 00000-0 90000-4 0 28 > 2 26934 97.9250 105.5870 0354827 0.1152 0.0078 14.74316830 15 ----------------------------------------------------------------- To unsubscribe from SeeSat-L, send a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@satobs.org List archived at http://www.satobs.org/seesat/seesatindex.html
This archive was generated by hypermail 2b29 : Fri Dec 26 2003 - 17:26:14 EST