Names | NOAA-L | ||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Mission type | Weather | ||||||||||||||||||
Operator | NOAA | ||||||||||||||||||
COSPAR ID | 2000-055A | ||||||||||||||||||
SATCAT no. | 26536 | ||||||||||||||||||
Mission duration | 2 years (planned)[1] 13.75 years (achieved) | ||||||||||||||||||
Spacecraft properties | |||||||||||||||||||
Spacecraft type | TIROS | ||||||||||||||||||
Bus | Advanced TIROS-N | ||||||||||||||||||
Manufacturer | Lockheed Martin | ||||||||||||||||||
Launch mass | 2,232 kg (4,921 lb)[2] | ||||||||||||||||||
Dry mass | 1,479 kg (3,261 lb) | ||||||||||||||||||
Power | 833 watts[2] | ||||||||||||||||||
Start of mission | |||||||||||||||||||
Launch date | 21 September 2000, 10:22:00 UTC[3] | ||||||||||||||||||
Rocket | Titan 23G Star-37XFP-ISS (Titan 23G S/N G-13) | ||||||||||||||||||
Launch site | Vandenberg, SLC-4W | ||||||||||||||||||
Contractor | Lockheed Martin | ||||||||||||||||||
End of mission | |||||||||||||||||||
Disposal | Decommissioned | ||||||||||||||||||
Deactivated | 9 June 2014 | ||||||||||||||||||
Destroyed | 25 November 2015 | ||||||||||||||||||
Last contact | 6 June 2014 | ||||||||||||||||||
Orbital parameters | |||||||||||||||||||
Reference system | Geocentric orbit[4] | ||||||||||||||||||
Regime | Sun-synchronous orbit | ||||||||||||||||||
Perigee altitude | 843 km (524 mi) | ||||||||||||||||||
Apogee altitude | 850 km (530 mi) | ||||||||||||||||||
Inclination | 98.80° | ||||||||||||||||||
Period | 102.10 minutes | ||||||||||||||||||
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NOAA-16, also known as NOAA-L before launch, was an operational, polar orbiting, weather satellite series (NOAA K-N) operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-16 continued the series of Advanced TIROS-N (ATN) spacecraft that began with the launch of NOAA-8 (NOAA-E) in 1983; but it had additional new and improved instrumentation over the NOAA A-K series and a new launch vehicle (Titan 23G).[5] It was launched on 21 September 2000 and, following an unknown anomaly, it was decommissioned on 9 June 2014. In November of 2015 it broke up in orbit, creating more than 200 pieces of debris.
Trajectory
was invoked but never defined (see the help page).