Nilesat 1 96666U 980xx A 98118.96737500 .00000004 00000-0 00000-0 0 12 2 96666 7.0000 16.8770 7308880 178.0010 2.2770 2.27200000 03 This is based upon the info below and should not suffer from my typical prelaunch analysis since it launched over two hours ago :) Ron Lee At 10:48 AM 4/28/98 -0700, you wrote: >NOMINAL ORBITS > NILESAT BSAT >EPOCH (D/HH:MM:SS.SSS): 118/23:14:13.220 118/23:18:39.220 >PERIOD (MIN): 633.887 633.627 >INCLINATION (DEG): 7.000 6.997 >ECCENTRICITY (DEG): 0.730888 0.730769 >SEMI-MAJOR AXIS (KM): 24443.7658 24437.0824 >ARGUMENT OF PERIGEE (DEG): 178.001 178.051 >RA OF ASCENDING NODE (DEG): 16.877 16.865 >MEAN ANOMALY (DEG): 2.277 4.793 >START ORBIT TIME (HHH:MM:SS.SSS)MET:000:21:13.220 000:25:39.220 >END ORBIT TIME (HHH:MM:SS.SSS)MET: 022:00:00.000 022:00:00.000 >HEIGHT (KM): 348.3080 931.0474 >INJECTION LATITUDE (DEG): 2.15S 4.406S >INJECTION LONGITUDE (DEG): 9.30E 29.147E >INJECTION INERTIAL AZIMUTH (DEG): 96.657 95.448 >INJECTION TIME (D/HH:MM:SS.SSS): 118/23:14:13.220 118/23:18:39.220 > >Launch is tonight 2253 UTC. > > >Keith Stein >Associate Technical Editor > >Launchspace Publications, Inc. >http://www.launchspace.com >(703) 749-2324, ext 114 >(703) 749-3177 (fax) > > >