At 09:31UT, a Proton-M with a Briz-M upper stage will launch the ExoMars-2016 mission. The mission will follow the typical Briz insertion profile of 4 burns with intermediate orbits. I have not been able to find exact information about the burn profile. Approximate information is provided at these two links: http://www.russianspaceweb.com/exomars2016-launch.html http://blogs.esa.int/rocketscience/2016/03/13/why-exomars-ride-to-space-takes-the-time-it-does/ Using that information, I estimate the following TLEs: Parking orbit 1 85001U 16074.39701389 .00000000 00000-0 50000-4 0 04 2 85001 51.5500 323.0000 0000000 0.0000 50.0000 16.36550117 00 Intermediate orbit 1 85002U 16074.46527778 .00000000 00000-0 00000-0 0 02 2 85002 51.5500 323.0000 2951143 90.0000 0.0000 9.52124987 02 Transfer orbit 1 85003U 16074.57013889 .00000000 00000-0 00000-0 0 08 2 85003 51.5500 323.0000 6101816 90.0000 0.0000 3.91570020 01 Earth escape orbit 1 85004U 16074.82638889 .00000000 00000-0 00000-0 0 00 2 85004 51.5500 323.0000 9186763 90.0000 359.0000 0.37311395 01 The 85001 elset is valid from 09:31 to 11:10UT. Then the 85002 elset should be used until it reaches perigee at 13:41UT. After that the 85003 elset is valid until the 19:50UT perigee. After that the 85004 elset is approximate; ExoMars will be on a hyperbolic orbit with respect to the Earth, but since two-line-elements only support eccentric orbits the 85004 elset will only be valid for the first few hours after the 4th Briz-M burn. ExoMars will be visible in the transfer orbit (85003) from Australia, and then shortly after the last Briz-M burn from the European and African continents. Note that the elements above are very approximate, so allow for large offsets in time and position. If more information about the orbits becomes available I will try to provide updated orbits. Regards, Cees _______________________________________________ Seesat-l mailing list http://mailman.satobs.org/mailman/listinfo/seesat-lReceived on Mon Mar 14 2016 - 04:29:20 UTC
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