10.03 revs/day is too high for the intended orbit. The inclination is also too high. Ron Lee > > AMC-16 > 1 28472U 04048A 04352.48218405 .00000424 -93139-6 00000+0 0 10 > 2 28472 27.1980 91.2197 2792904 145.1210 235.9961 10.03169321 09 > > It was planed to be put into the following geo transfer orbit according to ILS. > > Orbital Parameters(@ Separation): > > Apogee Altitude: 19,323 nm (35,786 km) > > Perigee Altitude: 2591 nm (4,798 km) > > Inclination: 18.02 deg > > Good soon another geo sat to observe:) > > Kevin > > > > __________________________________ > Do you Yahoo!? > Read only the mail you want - Yahoo! Mail SpamGuard. > http://promotions.yahoo.com/new_mail > > ------------------------------------------------------------------------- > Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: > http://www.satobs.org/seesat/seesatindex.html > --------------------------------------------- This message was sent using Endymion MailMan. http://www.endymion.com/products/mailman/ ------------------------------------------------------------------------- Subscribe/Unsubscribe info, Frequently Asked Questions, SeeSat-L archive: http://www.satobs.org/seesat/seesatindex.html
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