The following elements were displayed during the launch coverage: MECO1: apogee 561.5 nm, perigee 95.7 nm, eccentricity 0.061729, inclination 27.487, RA of ascending node 301.960, argument of perigee 162.745 Near spacecraft separation: apogee 27030 nm, perigee 121 nm, eccentricity 0.7905, inclination 20.52, Ra of ascending node 301.455, argument of perigee 179.986 The latter is pretty close to Ted's prediction for AEHF3. Regards, Cees _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-l
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