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GOES 15

ResourceID
spase://SMWG/Observatory/GOES/15

Description

GOES 15, also known as GOES-P, is an American (NOAA) geostationary weather satellite that was launched by a Delta 4 rocket from Cape Canaveral on 04 March 2010 at 23:57 UT. It is the third in an updated series of Geostationary Operational Environmental Satellites which carry an imager, sounder, the Solar X-ray Imager (SXI), the Space Environment Monitor System (SEM) and a search and rescue transponder which relays distress signals to the ground. The SEM consists of two magnetometers; an Energetic Particle Sensor (EPS) composed of a High-Energy Proton and Alpha Detector (HEPAD), a Magnetosphere Electron Detector (MAGED), an Energetic Proton Electron and Alpha Detector (EPEAD), and a Magnetosphere Proton Detector (MAGPD); Energetic X-Ray Sensor (XRS) and Extreme Ultraviolet (EUV) sensors. GOES 15 was placed in orbit originally as a spare and has an expected mission lifetime of 10 years (2 years on-orbit storage and 8 years operational).

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Details

Version:2.7.1

Observatory

ResourceID
spase://SMWG/Observatory/GOES/15
ResourceHeader
ResourceName
GOES 15
AlternateName
Geostationary Operational Environmental Satellite 15
AlternateName
2010-008A
AlternateName
GOES P
ReleaseDate
2026-07-20 16:23:10Z
RevisionHistory
RevisionEvent
ReleaseDate
2019-05-05 12:34:56Z
Note
Only known prior ReleaseDate of the metadata
RevisionEvent
ReleaseDate
2026-07-20 16:23:10Z
Note
Added HelioData InformationURL, Updated to SPASE Version 2.7.1. JWL
Description

GOES 15, also known as GOES-P, is an American (NOAA) geostationary weather satellite that was launched by a Delta 4 rocket from Cape Canaveral on 04 March 2010 at 23:57 UT. It is the third in an updated series of Geostationary Operational Environmental Satellites which carry an imager, sounder, the Solar X-ray Imager (SXI), the Space Environment Monitor System (SEM) and a search and rescue transponder which relays distress signals to the ground. The SEM consists of two magnetometers; an Energetic Particle Sensor (EPS) composed of a High-Energy Proton and Alpha Detector (HEPAD), a Magnetosphere Electron Detector (MAGED), an Energetic Proton Electron and Alpha Detector (EPEAD), and a Magnetosphere Proton Detector (MAGPD); Energetic X-Ray Sensor (XRS) and Extreme Ultraviolet (EUV) sensors. GOES 15 was placed in orbit originally as a spare and has an expected mission lifetime of 10 years (2 years on-orbit storage and 8 years operational).

Acknowledgement
National Aeronautics and Space Administration
Contacts
RolePersonStartDateStopDateNote
1.GeneralContactspase://SMWG/Person/UNKNOWN
InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the GOES 15 mission

InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the GOES 15 mission

InformationURL
Name
HelioData
URL
Description

The HelioData mission page provides an overview of the mission and more, such as all SPASE dataset records associated with it.

PriorIDs
spase://SMWG/Observatory/GOES/15
ObservatoryGroupID
Location
ObservatoryRegion
Earth.Magnetosphere.Main