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.
Version:2.3.1
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.
| Role | Person | |
|---|---|---|
| 1. | PrincipalInvestigator | spase://SMWG/Person/Christopher.T.Russell |
| 2. | DataProducer | spase://SMWG/Person/Robert.J.Strangeway |
ftp access to CDF files
In CDF via HTTP from SPDF
Plots, lists and files from CDAWeb
DD-MON-YY HH:MM:SS.SSS
Triaxial magnetic field vector in spacecraft coordinates (SC)
The three elements are BX, BY, BZ
Magnetic field magnitude
Triaxial magnetic field vector in GSM coordinates
The three elements are BX, BY, BZ
Triaxial magnetic field vector in GSM coordinates
The three elements are BX, BY, BZ
Standard deviations in the field component averages
in SC coordinates
The three elements are the standard deviations
in BX, BY, BZ (SC coordinates) averages
Standard deviations in the field magnitude averages
Difference between magnitudes of model internal field
and observed field
Difference between magnitudes of model internal field
and observed field
Difference between GSM components of model internal field
and observed field
GSM X,Y,Z components of model internal field
vector minus observed field vector
Difference between magnitudes of model internal plus
external field and observed field
Difference between GSM components of model internal
plus external field and observed field
GSM X,Y,Z components of model internal plus
external field vector minus observed field vector
Geocentric distance of spacecraft, in Earth radii
Spacecraft position vector, GSM Cartesian
components, in Earth radii
GSM X,Y,Z components of spacecraft
position vector
Spacecraft position vector, GSE Cartesian
components, in Earth radii
GSE X,Y,Z components of spacecraft
position vector
Clock angle from Y GSM axis, positive toward +Z GSM
GSE X component of the vector that starts
at the spacecraft and intersects the model magnetopause
perpendicularly
GSE Y component of the vector that starts
at the spacecraft and intersects the model magnetopause
perpendicularly
GSE Z component of the vector that starts
at the spacecraft and intersects the model magnetopause
perpendicularly
Component of the ISEE_1-ISEE_2
separation vector along the vector that starts at the
spacecraft and intersects the model magnetopause
perpendicularly
GSE X component of the vector that starts
at the spacecraft and intersects the model bow shock
perpendicularly
GSE Y component of the vector that starts
at the spacecraft and intersects the model bow shock
perpendicularly
GSE Z component of the vector that starts
at the spacecraft and intersects the model bow shock
perpendicularly
Component of the ISEE_1-ISEE_2
separation vector along the vector that starts at the
spacecraft and intersects the model bow shock
perpendicularly