NOAA-20

NOAA-20, designated JPSS-1 prior to launch, is the first of the United States National Oceanic and Atmospheric Administration's latest generation of U.S. polar-orbiting, non-geosynchronous, environmental satellites called the Joint Polar Satellite System. NOAA-20 was launched on 18 November 2017 and joined the Suomi National Polar-orbiting Partnership satellite in the same orbit. NOAA-20 operates about 50 minutes behind Suomi NPP, allowing important overlap in observational coverage. Circling the Earth from pole-to-pole, it crosses the equator about 14 times daily, providing full global coverage twice a day. This gives meteorologists information on "atmospheric temperature and moisture, clouds, sea-surface temperature, ocean color, sea ice cover, volcanic ash, and fire detection" so as to enhance weather forecasting including hurricane tracking, post-hurricane recovery by detailing storm damage and mapping of power outages.

NOAA-20
Artist illustration of the NOAA-20 satellite
NamesJPSS-1
Mission typeWeather
OperatorNOAA
COSPAR ID2017-073A
SATCAT no.43013
Websitehttp://www.jpss.noaa.gov/
Mission duration7 years (planned)
6 years, 2 months, 23 days (elapsed)
Spacecraft properties
Spacecraft typeJoint Polar Satellite System-1
BusBCP-2000
ManufacturerBall Aerospace & Technologies
Launch mass2540 kg
Dry mass1929 kg
Payload mass578 kg
Dimensions1.3 m x 1.3 m x 4.2 m
Power1932 watts
Start of mission
Launch date18 November 2017,
09:47:36 UTC
RocketDelta II 7920-10C
(Delta D378)
Launch siteVandenberg, SLC-2W
ContractorUnited Launch Alliance
Entered service30 May 2018
Orbital parameters
Reference systemGeocentric orbit
RegimeSun-synchronous orbit
Perigee altitude824.3 km (512.2 mi)
Apogee altitude833.0 km (517.6 mi)
Inclination98.79°
Period101.44 minutes
 

The project incorporates five instruments, and these are substantially upgraded since previous satellite equipment. The project's greater-detailed observations provide better predictions and emphasize climate behavior in cases like El Niño and La Niña.

The satellite bus of the project and Ozone Mapping and Profiler Suite (OMPS) equipment, was designed by Ball Aerospace & Technologies. The Visible Infrared Imaging Radiometer Suite (VIIRS) and the Common Ground System (CGS) were built by Raytheon Company, and the Cross-track Infrared Sounder (CrIS) was by Harris Corporation. The Advanced Technology Microwave Sounder (ATMS) and the Clouds and the Earth's Radiant Energy System (CERES) instrument were built by Northrop Grumman Innovation Systems.

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