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ISEE 2 magnetometer 1-min data

(1987). ISEE 2 magnetometer 1-min data [Data set]. University of California, Los Angeles and NASA Space Physics Data Facility. https://doi.org/10.21978/p8t923 (CiteAs link). Accessed on .

ResourceID
spase://NASA/NumericalData/ISEE2/MAG/PT1M

Description

This data set contains magnetic field component and magnitude averages every minute, with components given in spacecraft, GSE and GSM coordinates. Standard deviations in the averages are given, as are differences between the averages and model field vectors. Geocentric (GSE and GSM) spacecraft position information is given, as is ISEE1-ISEE2 separation vector information. ISEE 2 spin vector direction and ISEE 2 velocity vector information, relative to the Earth and to ISEE 1, are given. Miscellaneous other parameters are also given.

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Details

Version:2.3.2

NumericalData

ResourceID
spase://NASA/NumericalData/ISEE2/MAG/PT1M
ResourceHeader
ResourceName
ISEE 2 magnetometer 1-min data
DOI
https://doi.org/10.21978/p8t923
ReleaseDate
2021-05-31 12:34:56.789
RevisionHistory
RevisionEvent
ReleaseDate
2021-05-31 12:34:56.789
Note
Updated to SPASE Version 2.3.2 if needed, Applied quality control for DOI usage, LFB
Description

This data set contains magnetic field component and magnitude averages every minute, with components given in spacecraft, GSE and GSM coordinates. Standard deviations in the averages are given, as are differences between the averages and model field vectors. Geocentric (GSE and GSM) spacecraft position information is given, as is ISEE1-ISEE2 separation vector information. ISEE 2 spin vector direction and ISEE 2 velocity vector information, relative to the Earth and to ISEE 1, are given. Miscellaneous other parameters are also given.

Acknowledgement
ISEE Magnetometer Team at UCLA/IGPP and the CDAWeb team at NASA/GSFC
PublicationInfo
Authors
Russell, Christopher T.
PublicationDate
1987-01-01 00:00:00
PublishedBy
University of California, Los Angeles and NASA Space Physics Data Facility
Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Christopher.T.Russell
2.DataProducerspase://SMWG/Person/Robert.J.Strangeway
PriorIDs
spase://VMO/NumericalData/ISEE2/MAG/PT1M
spase://VSPO/NumericalData/ISEE2/MAG/PT1M
AccessInformation
RepositoryID
spase://SMWG/Repository/NASA/GSFC/SPDF
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
ftps://spdf.gsfc.nasa.gov/pub/data/isee/isee2/isee2_cdaweb/60sec_mfi/
Description

ftp access to CDF files

AccessURL
Name
HTTPS from SPDF
URL
https://spdf.gsfc.nasa.gov/pub/data/isee/isee2/isee2_cdaweb/60sec_mfi/
Description

In CDF via HTTP from SPDF

Format
CDF
Acknowledgement
UCLA ISEE Magnetometer and GSFC CDAWeb teams
AccessInformation
RepositoryID
spase://SMWG/Repository/NASA/GSFC/SPDF/CDAWeb
AccessRights
Open
AccessURL
Name
CDAWeb
URL
https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=ISEE2_60SEC_MFI&index=sp_phys
ProductKey
ISEE2_60SEC_MFI
Description

Plots, lists and files from CDAWeb

Format
Text
Acknowledgement
UCLA ISEE Magnetometer and GSFC CDAWeb teams
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
ISEE2_60SEC_MFI
Description

Web Service to this product using the HAPI interface.

Format
CSV
Acknowledgement
UCLA ISEE Magnetometer and GSFC CDAWeb teams
ProcessingLevel
Calibrated
InstrumentIDs
spase://SMWG/Instrument/ISEE2/MAG
MeasurementType
MagneticField
TemporalDescription
TimeSpan
StartDate
1977-10-22 21:04:19
StopDate
1987-09-26 16:10:30
Cadence
PT1M
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Heliosphere.NearEarth
Parameter #1
Name
Universal Time
ParameterKey
Epoch
Description

DD-MON-YY HH:MM:SS.SSS

Support
SupportQuantity
Temporal
Parameter #2
Name
Magnetic Field Vector, SC Coordinates
ParameterKey
BX, BY, BZ
Description

Triaxial magnetic field vector in spacecraft coordinates (SC)

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
SC
Structure
Size
3
Description

The three elements are BX, BY, BZ

Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #3
Name
Magnetic Field Magnitude
ParameterKey
BTOT
Description

Magnetic field magnitude

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
Field
Qualifier
Magnitude
FieldQuantity
Magnetic
Parameter #4
Name
Magnetic Field Vector, GSM Coordinates
ParameterKey
BX_GSM, BY_GSM, BZ_GSM
Description

Triaxial magnetic field vector in GSM coordinates

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Description

The three elements are BX, BY, BZ

Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #5
Name
Magnetic Field Vector, GSE Coordinates
ParameterKey
BX_GSE, BY_GSE, BZ_GSE
Description

Triaxial magnetic field vector in GSM coordinates

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Structure
Size
3
Description

The three elements are BX, BY, BZ

Field
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #6
Name
Standard Deviations in field component averages
ParameterKey
SDX, SDY, SDZ
Description

Standard deviations in the field component averages in SC coordinates

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
SC
Structure
Size
3
Description

The three elements are the standard deviations in BX, BY, BZ (SC coordinates) averages

Field
Qualifier
StandardDeviation
Qualifier
Vector
FieldQuantity
Magnetic
Parameter #7
Name
Standard Deviations in field magnitude averages
ParameterKey
SDT
Description

Standard deviations in the field magnitude averages

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
Field
Qualifier
StandardDeviation
Qualifier
Magnitude
FieldQuantity
Magnetic
Parameter #8
Name
Composite Standard Deviations in field average
ParameterKey
SDC
Description

Difference between magnitudes of model internal field and observed field

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
Field
Qualifier
StandardDeviation
FieldQuantity
Magnetic
Parameter #9
Name
Model internal field minus observed field, magnitudes
ParameterKey
BINT
Description

Difference between magnitudes of model internal field and observed field

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
Field
Qualifier
Deviation
Qualifier
Magnitude
FieldQuantity
Magnetic
Parameter #10
Name
Model internal field minus observed field, GSM components
ParameterKey
BXIM_GSM, BYIM_GSM, BZIM_GSM
Description

Difference between GSM components of model internal field and observed field

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Description

GSM X,Y,Z components of model internal field vector minus observed field vector

Field
Qualifier
Deviation
Qualifier
Component
FieldQuantity
Magnetic
Parameter #11
Name
Model internal plus external field minus observed field, magnitudes
ParameterKey
BINTEXT
Description

Difference between magnitudes of model internal plus external field and observed field

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
Field
Qualifier
Deviation
Qualifier
Magnitude
FieldQuantity
Magnetic
Parameter #12
Name
Model internal plus external field minus observed field, GSM components
ParameterKey
BXIE_GSM, BYIE_GSM, BZIE_GSM
Description

Difference between GSM components of model internal plus external field and observed field

Cadence
PT1M
Units
nT
UnitsConversion
1.0E-9>T
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Description

GSM X,Y,Z components of model internal plus external field vector minus observed field vector

Field
Qualifier
Deviation
Qualifier
Component
FieldQuantity
Magnetic
Parameter #13
Name
Geocentric distance of spacecraft
ParameterKey
R
Description

Geocentric distance of spacecraft, in Earth radii

Cadence
PT1M
Units
Re
Support
SupportQuantity
Positional
Parameter #14
Name
Spacecraft position vector, GSM
ParameterKey
X_GSM, Y_GSM, Z_GSM
Description

Spacecraft position vector, GSM Cartesian components, in Earth radii

Cadence
PT1M
Units
Re
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Description

GSM X,Y,Z components of spacecraft position vector

Support
SupportQuantity
Positional
Parameter #15
Name
Spacecraft position vector, GSE
ParameterKey
X_GSE, Y_GSE, Z_GSE
Description

Spacecraft position vector, GSE Cartesian components, in Earth radii

Cadence
PT1M
Units
Re
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Structure
Size
3
Description

GSE X,Y,Z components of spacecraft position vector

Support
SupportQuantity
Positional
Parameter #16
Name
Z position of nominal Russell Brody neutral sheet, GSM
ParameterKey
ZNS_GSM
Support
SupportQuantity
Positional
Parameter #17
Name
Dipole tilt angle
ParameterKey
TILT
Support
SupportQuantity
Positional
Parameter #18
Name
L Shell parameter
ParameterKey
L
Support
SupportQuantity
Positional
Parameter #19
Name
Local time
ParameterKey
Local_time
Support
SupportQuantity
Positional
Parameter #20
Name
Magnetic latitude
ParameterKey
MLAT
Support
SupportQuantity
Positional
Parameter #21
Name
Sun-Earth-Satellite angle
ParameterKey
SES
Support
SupportQuantity
Positional
Parameter #22
Name
Clock angle
ParameterKey
PHI
Description

Clock angle from Y GSM axis, positive toward +Z GSM

Support
SupportQuantity
Positional
Parameter #23
Name
Spacecraft spin period
ParameterKey
SPIN
Support
SupportQuantity
Positional
Parameter #24
Name
GSM longitude of spin axis
ParameterKey
SLNG_GSM
Support
SupportQuantity
Positional
Parameter #25
Name
GSM latitude of spin axis
ParameterKey
SLT_GSM
Support
SupportQuantity
Positional
Parameter #26
Name
GSE longitude of spin axis
ParameterKey
SLNG_GSE
Support
SupportQuantity
Positional
Parameter #27
Name
GSE latitude of spin axis
ParameterKey
SLT_GSE
Support
SupportQuantity
Positional
Parameter #28
Name
GSM X component of spacecraft velocity
ParameterKey
VX_GSM
Support
SupportQuantity
Positional
Parameter #29
Name
GSM Y component of spacecraft velocity
ParameterKey
VY_GSM
Support
SupportQuantity
Positional
Parameter #30
Name
GSM Z component of spacecraft velocity
ParameterKey
VZ_GSM
Support
SupportQuantity
Positional
Parameter #31
Name
Spacecraft speed
ParameterKey
V
Support
SupportQuantity
Positional
Parameter #32
Name
GSM X component of ISEE 1 velocity relative to ISEE 2
ParameterKey
DVX_GSM
Support
SupportQuantity
Positional
Parameter #33
Name
GSM Y component of ISEE 1 velocity relative to ISEE 2
ParameterKey
DVY_GSM
Support
SupportQuantity
Positional
Parameter #34
Name
GSM Z component of ISEE 1 velocity relative to ISEE 2
ParameterKey
DVZ_GSM
Support
SupportQuantity
Positional
Parameter #35
Name
ISEE 1 speed relative to ISEE 2
ParameterKey
DV
Support
SupportQuantity
Positional
Parameter #36
Name
GSM X separation of ISEE 2 to ISEE 1
ParameterKey
DX_GSM
Support
SupportQuantity
Positional
Parameter #37
Name
GSM Y separation of ISEE 2 to ISEE 1
ParameterKey
DY_GSM
Support
SupportQuantity
Positional
Parameter #38
Name
GSM Z separation of ISEE 2 to ISEE 1
ParameterKey
DZ_GSM
Support
SupportQuantity
Positional
Parameter #39
Name
GSE X separation of ISEE 2 to ISEE 1
ParameterKey
DX_GSE
Support
SupportQuantity
Positional
Parameter #40
Name
GSE Y separation of ISEE 2 to ISEE 1
ParameterKey
DY_GSE
Support
SupportQuantity
Positional
Parameter #41
Name
GSE Z separation of ISEE 2 to ISEE 1
ParameterKey
DZ_GSE
Support
SupportQuantity
Positional
Parameter #42
Name
Distance between ISEE 2 to ISEE 1
ParameterKey
DR
Support
SupportQuantity
Positional
Parameter #43
Name
GSE X component of vector to magnetopause
ParameterKey
NMPX_GSE
Description

GSE X component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly

Support
SupportQuantity
Positional
Parameter #44
Name
GSE Y component of vector to magnetopause
ParameterKey
NMPY_GSE
Description

GSE Y component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly

Support
SupportQuantity
Positional
Parameter #45
Name
GSE Z component of vector to magnetopause
ParameterKey
NMPZ_GSE
Description

GSE Z component of the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly

Support
SupportQuantity
Positional
Parameter #46
Name
Component of ISEE_1-ISEE_2 vector, MP
ParameterKey
MPS
Description

Component of the ISEE_1-ISEE_2 separation vector along the vector that starts at the spacecraft and intersects the model magnetopause perpendicularly

Support
SupportQuantity
Positional
Parameter #47
Name
GSE X component of vector to bow shock
ParameterKey
NSX_GSE
Description

GSE X component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly

Support
SupportQuantity
Positional
Parameter #48
Name
GSE Y component of vector to bow shock
ParameterKey
NSY_GSE
Description

GSE Y component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly

Support
SupportQuantity
Positional
Parameter #49
Name
GSE Z component of vector to bow shock
ParameterKey
NSZ_GSE
Description

GSE Z component of the vector that starts at the spacecraft and intersects the model bow shock perpendicularly

Support
SupportQuantity
Positional
Parameter #50
Name
Component of ISEE_1-ISEE_2 vector, BS
ParameterKey
MPS
Description

Component of the ISEE_1-ISEE_2 separation vector along the vector that starts at the spacecraft and intersects the model bow shock perpendicularly

Support
SupportQuantity
Positional