Names | NOAA-F | ||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Mission type | Weather | ||||||||||||||||
Operator | NOAA | ||||||||||||||||
COSPAR ID | 1984-123A | ||||||||||||||||
SATCAT no. | 15427 | ||||||||||||||||
Mission duration | 2 years (planned) 13 years (achieved) | ||||||||||||||||
Spacecraft properties | |||||||||||||||||
Spacecraft type | TIROS | ||||||||||||||||
Bus | Advanced TIROS-N | ||||||||||||||||
Manufacturer | GE Aerospace | ||||||||||||||||
Launch mass | 1,420 kg (3,130 lb) [1] | ||||||||||||||||
Dry mass | 740 kg (1,630 lb) | ||||||||||||||||
Start of mission | |||||||||||||||||
Launch date | 12 December 1984, 10:42:00 UTC | ||||||||||||||||
Rocket | Atlas-E Star-37S-ISS (Atlas S/N 39E) | ||||||||||||||||
Launch site | Vandenberg, SLC-3W | ||||||||||||||||
Contractor | Convair | ||||||||||||||||
End of mission | |||||||||||||||||
Disposal | Decommissioned | ||||||||||||||||
Last contact | 13 February 1998 [2] | ||||||||||||||||
Orbital parameters | |||||||||||||||||
Reference system | Geocentric orbit[3] | ||||||||||||||||
Regime | Sun-synchronous orbit | ||||||||||||||||
Perigee altitude | 841 km (523 mi) | ||||||||||||||||
Apogee altitude | 862 km (536 mi) | ||||||||||||||||
Inclination | 99.17° | ||||||||||||||||
Period | 102.0 minutes | ||||||||||||||||
| |||||||||||||||||
NOAA-9, known as NOAA-F before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Environmental Satellite Data and Information Service (NESDIS). It was the second of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.[4]