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Launch Schedules

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   NOAA POES 17 (M) - Summary
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The 2232 kg (4919 lbm) satellite is the latest in the series of advanced TIROS-N spacecraft that provide a platform to support the environmental monitoring instruments for imaging and measuring the Earth's atmosphere, its surface and cloud cover. The spacecraft is the second in a series of five Polar Operational Environmental Satellites (POES) to be built by Lockheed Martin Space Systems Company, Sunnyvale, CA. The operational system consists of two polar-orbiting satellites. The polar-orbiting spacecraft serve as complementary satellites to the geosynchronous Geostationary Operational Environmental Satellites (GOES) system. NOAA M also provides a platform for the Search and Rescue Satellite Aided Tracking system, part of the COSPAS-SARSAT constellation. The Search and Rescue satellites (SARSAT/COSPAR) have been instrumental in saving more than 13,000 lives since the inception of the system.

The instruments onboard the satellite include the Advanced Very High Resolution Radiometer (AVHRR/3), the High Resolution Infrared Radiation Sounder (HIRS/3), the Advanced Microwave Sounding Unit-A (AMSU-A1, A2), the AMSU-B, the Solar Backscatter Ultraviolet Radiometer (SBUV/2), the Space Environment Monitor (SEM/2) and the Data Collection System (DCS/2). The AVHRR/3 is the primary imaging system, which consists of visible, near infrared (IR) and thermal IR channels. The primary sounding suite is the HIRS/3, AMSU-A and AMSU-B, which measures atmospheric temperature and humidity. The SBUV/2 instrument is both an imager and a sounder. As an imager, it produces total column ozone maps. As a sounder, it obtains and measures the ozone distribution in the atmosphere as a function of altitude.

In addition to the weather instruments, the satellite carries two search and rescue instruments, the Search and Rescue Repeater (SARR) and the Search and Rescue Processor (SARP).

NOAA POES 17 (M)
National Oceanic and Atmospheric Administration
Polar Operational Environmental Satellite

SPACECRAFT

Int'l Designation

2002 032A

Launched

Owner / Sponsor U.S. National Oceanic and Atmospheric Administration (NOAA)
Mission Weather observation
Manufacturer Lockheed Martin  
Launch Mass 2232 kg (4919 lbm)
Dimensions, stowed  
Mission Orbit LEO - 833 km (450 nmi)

98.7465°

Design Life 2 years
Power (EOL)  
Other names NOAA M

LAUNCH

Launch Vehicle Model Titan II
Date / Time (UTC) 24 June 2002

18:23:03.656

FINANCIAL

Satellite cost US$202 million
Web Links  

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