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GOES 9 Space Environment Monitor (SEM) Triaxial Fluxgate Magnetometer (FGM), Magnetic Field and Ephemeris, Multiple Coordinate Systems, 1.0 min Data

ResourceID
spase://NOAA/NumericalData/GOES/9/MAG/PT1M

Description

The NOAA Geostationary Operational Environment Satellite (GOES) key parameters. This data is a subset of the data available from the GOES Space Environment Monitor (SEM) instruments. It contains vector magnetic field in three coordinate systems:

  • Spacecraft P,E,N
  • GSM X,Y,Z
  • GSE X,Y,Z

Spacecraft magnetic field is defined as:

  • P perpendicular to the spacecraft orbital plane or parallel to the spin axis of the Earth in the case of a 0° inclination orbit
  • E perpendicular to P and directed earthward
  • N perpendicular to both P and E and directed eastward

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Details

Version:2.3.0

NumericalData

ResourceID
spase://NOAA/NumericalData/GOES/9/MAG/PT1M
ResourceHeader
ResourceName
GOES 9 Space Environment Monitor (SEM) Triaxial Fluxgate Magnetometer (FGM), Magnetic Field and Ephemeris, Multiple Coordinate Systems, 1.0 min Data
ReleaseDate
2021-04-27 17:52:57Z
Description

The NOAA Geostationary Operational Environment Satellite (GOES) key parameters. This data is a subset of the data available from the GOES Space Environment Monitor (SEM) instruments. It contains vector magnetic field in three coordinate systems:

  • Spacecraft P,E,N
  • GSM X,Y,Z
  • GSE X,Y,Z

Spacecraft magnetic field is defined as:

  • P perpendicular to the spacecraft orbital plane or parallel to the spin axis of the Earth in the case of a 0° inclination orbit
  • E perpendicular to P and directed earthward
  • N perpendicular to both P and E and directed eastward
Acknowledgement
Users should acknowledge the CDAWeb for providing access to the data as well as the P.I. H. Singer and originating institution NOAA Space Environment Center
Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Howard.J.Singer
InformationURL
Name
Geostationary Satellite Server
URL
https://www.goes.noaa.gov/
Description

A web site hosted by NOAA with information and links to the GOES spacecraft and data

PriorIDs
spase://VMO/NumericalData/GOES9/MAG/PT1M
spase://VMO/NumericalData/GOES/9/MAG/PT1M
spase://VSPO/NumericalData/GOES/9/MAG/PT60S
spase://VSPO/NumericalData/GOES/9/MAG/PT1M
AccessInformation
RepositoryID
spase://SMWG/Repository/NASA/GSFC/SPDF
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
ftps://spdf.gsfc.nasa.gov/pub/data/goes/goes09/mag_k0/
AccessURL
Name
HTTPS from SPDF
URL
https://spdf.gsfc.nasa.gov/pub/data/goes/goes09/mag_k0/
Description

In CDF via HTTP from CDAWeb

AccessURL
Name
CDAWeb
URL
https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=G9_K0_MAG&index=sp_phys
ProductKey
G9_K0_MAG
Format
CDF
AccessInformation
RepositoryID
spase://SMWG/Repository/NASA/GSFC/SPDF
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
https://cdaweb.gsfc.nasa.gov/hapi
Style
HAPI
ProductKey
G9_K0_MAG
Description

Web Service to this product using the HAPI interface.

Format
CSV
ProviderResourceName
NOAA GOES 9
ProviderProcessingLevel
Level-2
ProviderVersion
4
InstrumentIDs
spase://SMWG/Instrument/GOES/9/MAG
spase://SMWG/Instrument/GOES/9/Ephemeris
MeasurementType
MagneticField
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1995-12-01 00:00:30
StopDate
1998-07-27 23:59:30
Cadence
PT1M
ObservedRegion
Earth.Magnetosphere
Keywords
Magnetic field
Parameter #1
Name
Epoch
ParameterKey
Epoch
Description

Epoch of the data point

Cadence
PT1M
Units
ms
ValidMin
1977-01-01T00:00:00
ValidMax
2010-12-31T23:59:59
FillValue
-1.0e+31
Support
SupportQuantity
Temporal
Parameter #2
Name
Time PB5
ParameterKey
Time_PB5
Description

Time array in the form: year, day of year, ms

Cadence
PT1M
ValidMin
1977-01-01T00:00:00
ValidMax
2010-12-31T23:59:59
FillValue
-2147483648
Support
SupportQuantity
Temporal
Parameter #3
Name
Magnetic Field Vector GSE
ParameterKey
B_GSE_c
Description

Magnetic Field vector in GSE coordinates

Cadence
PT1M
Units
nT
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Structure
Size
3
Element
Name
X, GSE
Qualifier
Component.I
Index
1
Element
Name
Y, GSE
Qualifier
Component.J
Index
2
Element
Name
Z, GSE
Qualifier
Component.K
Index
3
ValidMin
-600.0
ValidMax
600.0
FillValue
-1.0e+31
Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #4
Name
Magnetic Field vector GSM
ParameterKey
B_GSM_c
Description

Magnetic Field vector in GSM coordinates

Cadence
PT1M
Units
nT
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Element
Name
X, GSM
Qualifier
Component.I
Index
1
Element
Name
Y, GSM
Qualifier
Component.J
Index
2
Element
Name
Z, GSM
Qualifier
Component.K
Index
3
ValidMin
-600.0
ValidMax
600.0
FillValue
-1.0e+31
Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #5
Name
Magnetic Field vector spacecraft coordinates
ParameterKey
B_lcl_c
Description

Magnetic Field vector in spacecraft coordinates. Spacecraft magnetic field (P,E,N) is defined as:

  • P perpendicular to the spacecraft orbital plane or parallel to the spin axis of the Earth in the case of a 0° inclination orbit
  • E perpendicular to P and directed earthward
  • N perpendicular to both P and E and directed eastward
Cadence
PT1M
Units
nT
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
SpacecraftOrbitPlane
Structure
Size
3
Element
Name
P
Qualifier
Component.I
Index
1
Element
Name
E
Qualifier
Component.J
Index
2
Element
Name
N
Qualifier
Component.K
Index
3
ValidMin
-600.0
ValidMax
600.0
FillValue
-1.0e+31
Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #6
Name
Spacecraft Position Geographic
ParameterKey
SC_pos_ll
Description

Spacecraft position in Geographic coordinates

Cadence
PT1M
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEO
Structure
Size
3
Element
Name
Latitude
Qualifier
DirectionAngle.ElevationAngle
Index
1
Units
°
ValidMin
-90
ValidMax
90
Element
Name
Longitude
Qualifier
DirectionAngle.AzimuthAngle
Index
2
Units
°
ValidMin
0
ValidMax
360
Element
Name
Radius
Qualifier
Magnitude
Index
3
Units
km
ValidMin
50
ValidMax
50000
FillValue
-1.0e+31
Support
SupportQuantity
Positional
Parameter #7
Name
Spacecraft position GEO
ParameterKey
SC_pos_eo
Description

Spacecraft position in GEO coordinates

Cadence
PT1M
Units
km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GEO
Structure
Size
3
Element
Name
X, GEO
Qualifier
Component.I
Index
1
Element
Name
Y, GEO
Qualifier
Component.J
Index
2
Element
Name
Z, GEO
Qualifier
Component.K
Index
3
ValidMin
-5000.0
ValidMax
5000.0
FillValue
-1.0e+31
Support
SupportQuantity
Positional
Parameter #8
Name
Spacecraft Position GSE
ParameterKey
SC_pos_se
Description

Spacecraft position in GSE coordinates

Cadence
PT1M
Units
km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Structure
Size
3
Element
Name
GSE X
Index
1
Element
Name
GSE Y
Index
2
Element
Name
GSE Z
Index
3
ValidMin
-5000.0
ValidMax
5000.0
FillValue
-1.0e+31
Support
SupportQuantity
Positional
Parameter #9
Name
Spacecraft position GSM
ParameterKey
SC_pos_sm
Description

Spacecraft position in GSM coordinates

Cadence
PT1M
Units
km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Element
Name
X, GSM
Index
1
Element
Name
Y, GSM
Index
2
Element
Name
Z, GSM
Qualifier
Component.K
Index
3
ValidMin
-5000.0
ValidMax
5000.0
FillValue
-1.0e+31
Support
SupportQuantity
Positional
Parameter #10
Name
MGF Instrument Status
ParameterKey
MGF_stat
Description

Status of the magnetic field instrument:

  • 0 OK
  • 1 minor problem
  • 2 major problem
  • 3 missing data
Cadence
PT1M
Support
SupportQuantity
Other
Parameter #11
Name
Magnetic field post-gap flag
ParameterKey
B_flag
Description

Magnetic field data flag:

  • 0 no gap
  • 1 data not available
Cadence
PT1M
Support
SupportQuantity
Other
Parameter #12
Name
Spacecraft post-gap flag
ParameterKey
SC_flag
Description

Spacecraft location data flag:

  • 0 no gap
  • 1 data not available
Cadence
PT1M
Support
SupportQuantity
Other