Recently the orbit of Integral has been quoted as:- "Integral will be in a highly elliptical orbit with a perigee of 9,000km and apogee of 155,000km." I believe that first figure should be 90,000 and not 9,000. Can anyone confirm which is correct? Best wishes, Russell Eberst 55.9486N, 3.1383W, 150 feet = 46 metres above MSL ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www.satellite.eu.org/seesat/seesatindex.html
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