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 1 spin vector direction and ISEE 1 velocity vector information, relative to the Earth and to ISEE 2, are given. Miscellaneous other parameters are also given. Data are accessible as plots, lists and files from CDAWeb, and as CDF files from CDAWeb's ftp area.

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

Triaxial magnetic field vector in spacecraft coordinates (SC)

Magnetic field magnitude

Triaxial magnetic field vector in GSM coordinates

Triaxial magnetic field vector in GSM coordinates

Standard deviations in the field component averages in SC coordinates

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

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

Geocentric distance of spacecraft, in Earth radii

Spacecraft position vector, GSM Cartesian components, in Earth radii

Spacecraft position vector, GSE Cartesian components, in Earth radii

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