Hello all; In the previous message (http://www.satobs.org/seesat/Dec-2014/0068.html) Ted posted his orbit estimations. Some days ago I've made my own estimation as a test, with the help of Bob Christy from zarya.info. Here my estimations, based on the orbits that Ted computed for NROL-28 (later named USA-200) in 2008: This first elset is valid from about 14 minutes after launch, when the Centaur reaches positive perigee values and enters orbit: NROL-35 SECO1 192 X 2215 km 1 70000U 14500A 14346.14723380 0.00000000 00000-0 00000+0 0 07 2 70000 62.5000 207.6904 1333700 180.0001 2.1478 13.14740000 09 After that the Molniya orbit insertion should be made, with the separation of the payload: NROL-35 SECO2 1117 X 37641 km 1 70001U 14501A 14346.40070602 0.00000000 00000-0 00000+0 0 00 2 70001 62.4000 207.6544 7090000 266.5070 180.3826 2.10000000 03 Shortly after that a CCAM (Collision and Contamination Avoidance Maneuver) should be made to fit with the reentry NOTAM at 05:02:31 UTC (little bit less than 2 hours after liftoff). (Thanks to Ted Molczan who advised me that my original de-orbit elset was not correct): CENTAUR DE-ORBIT 2 -147 X 33546 km 1 70003U 14503A 14346.20973380 0.00000000 00000-0 00000+0 0 05 2 70003 62.3991 207.6803 7300128 258.1237 41.7968 2.47618863 07 *This elset may be rejected by some softwares as it has negative perigee. It should re-enter near the center of the NOTAM, at -48.74, 139.65. As ocurred with USA 200, the payload may up its perigee some days after launch. Hoewer Ted is much more experienced than I so his elsets should be more accurate than mine's. A difference between my elsets and his elsets can be watched. The differences are another inclination and a different RA of ascending node. Be good! Jon. -- Jon Mikel, COSPAR 6242, 42.9453, -2.82839, 623m, Bitoriano, Basque Country. _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-lReceived on Thu Dec 11 2014 - 12:09:25 UTC
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