C/NOFS
Space vehicle
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C/NOFS, or Communications/Navigation Outage Forecasting System was a USAF satellite developed by the Air Force Research Laboratory Space Vehicles Directorate to investigate and forecast scintillations in the Earth's ionosphere. Wikipedia
Launch date: April 16, 2008
Perigee altitude: 405 km (252 mi)
Launch mass: 384 kg (847 lb)
Mission duration: 3 years (planned); 7.5 years (achieved)
Reference system: Geocentric orbit
SATCAT no.: 32765