Ron Lee wrote: > 10.03 revs/day is too high for the intended orbit. The > inclination is also too high. That was the MECO1 orbit. This is the orbit of the Centaur after MECO2, which is also the transfer orbit of the payload: ATLAS V CENTAUR R/B 1 28473U 04048B 04352.67725183 .00000032 00000-0 00000+0 0 22 2 28473 18.0093 97.1846 5795458 0.2157 67.9484 1.99641666 06 1 28473U 04048B 04352.58255497 -.00000225 00000-0 00000+0 0 12 2 28473 18.2030 98.2346 5726110 358.2020 0.1232 2.06309776 02 Ted Molczan ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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