In view of Niel's comments I'm not sure what to think of this. It was posted a few days ago. I leave it as an exercise for the reader to convert these to TLEs, and verify that they correspond to actual launch times, and all that stuff. Richard Clark rclarke@ltpmail.gsfc.nasa.gov -------------------------------------------------------------------- STS-91 NOMINAL ORBITS MECO OMS-2 EPOCH (D/HH:MM:SS.SSS): 153/22:13:38.000 153/22:49:30.888 PERIOD (MIN): 88.319 90.184 INCLINATION (DEG): 51.653 51.674 ECCENTRICITY (DEG): 0.017851 0.005772 SEMI-MAJOR AXIS (KM): 6569.4506 6661.6167 ARGUMENT OF PERIGEE (DEG): 13.743 15.072 RA OF ASCENDING NODE (DEG): 119.017 118.865 MEAN ANOMALY (DEG): 35.313 180.117 START ORBIT TIME (HHH:MM:SS.SSS)MET: 000:08:39.000 000:44:31.888 END ORBIT TIME (HHH:MM:SS.SSS)MET: 000:44:31.888 003:00:00.000 HEIGHT (KM): 98.6579 324.5021 INJECTION LATITUDE (DEG): 37.22N 12.008S INJECTION LONGITUDE (DEG): 291.11E 74.910E INJECTION INERTIAL AZIMUTH (DEG): 51.015 140.685 INJECTION TIME (D/HH:MM:SS.SSS): 153/22:13:38.000 153/22:49:30.888 On Wed, 3 Jun 1998, Neil Clifford wrote: > Alexander Seidel scribbles: > > |>been fine, but he also saw nothing, despite clear skies. So the Shuttle, > |>on a somewhat lower track, probably entered shadow a fraction of a > |>minute before my output date. > > It entered eclipse approx. 2225 UTC (I was too busy explaining to > on-lookers to make notes). > > |>I wonder if there is a Pre-OMS elset around with which to calculate > |>the true situation well about 20 minutes in flight, approaching > |>Europe... Do you know? Do any others of the listees know? > > At one time it was possible to spirit pre OMS (post MECO) state vectors > out of JSC flight dynamics. But one day things changed and someone > somewhere decided that this was to be strictly verboten. With a little > bit of effort you could probably invent your own. > > -- > Neil Clifford * Oxford Starlink Computer Manager * clifford@astro.ox.ac.uk > >