3 sets of predicted elements for GPS launch May 17 at 0003 UT, this time with argument of perigee to give the correct apogee longitude. Since the first cutoff of the 2nd stage is not far from the perigee, the perigee height cannot be much less than 100km. For perigee 100km, 200 , 300km: 1 90002U 14000B 14136.99804000 .00000000 00000-0 00000+0 0 03 2 90002 55.0000 133.8000 6080500 80.0000 339.6317 4.09079200 08 1 90003U 14000C 14136.99788000 .00000000 00000-0 00000+0 0 05 2 90003 55.0000 133.8000 6032000 80.0000 339.2564 4.07217600 07 1 90004U 14000D 14136.99771000 .00000000 00000-0 00000+0 0 08 2 90004 55.0000 133.8000 5983800 80.0000 338.8813 4.05370600 00 Mike Waterman _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-lReceived on Fri May 16 2014 - 06:33:53 UTC
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