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Stay updated with the latest information on CBERS-3 and CBERS-4 satellite series, including launch details and payload specifications. Learn about the Sun-synchronous orbit characteristics and onboard storage capabilities. Follow the progress of these second-generation satellites set to be launched in December 2012.
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CBERS-3 Updates Julio Dalge – INPE Guo Chaohui – CRESDA SDCG Meeting – Reston, USA 2012
CBERS 3 & 4 – 2nd generation series Sun-synchronous orbit Altitude = 778 km Inclination = 98.5º Nodal period = 100.26 minutes Repeat cycle = 26 days Descending node at 10h30 local time
CBERS-3 will be launched in December 2012 Long-March 4 launching rocket will be used