Name: ISEE 2 magnetometer 1-min data
Creator: Russell, Christopher T.
Published: 1987-01-01
License: https://spdx.org/licenses/CC0-1.0.html

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} function getVersionedBibTeX(bibtex) { /* Add version field as suggested by August (Gus) Muench, Journals Data Editor, American Astronomical Society (email dated 7/7/25) */ const accessVersion = ", version={Accessed on " + currentIsoDateStr + "}"; const modifiedBibtex = bibtex.substring(0, bibtex.lastIndexOf("}")) + accessVersion + "}"; return modifiedBibtex; } function getBlob(text) { return new Blob([text], { type: "text/plain"}); } function clipboardAlert(text) { alert(text + "\nCopied to clipboard"); } function clipCitation(doi) { document.body.style.cursor = 'wait'; let url = "https://citation.doi.org/format?doi=" + doi.replace("https://doi.org/", "") + String.fromCodePoint(38) + "style=bibtex" + String.fromCodePoint(38) + "lang=en-US"; const text = new ClipboardItem({ "text/plain": fetch(url) .then(getResponseText) .then(getVersionedBibTeX) .then(getBlob) }); navigator.clipboard.write([text]); text.getType("text/plain") .then(getResponseText) .then(clipboardAlert); } function toggle_usa_banner_details() { const details = document.getElementById("usa-banner-details"); const indicator = document.getElementById("usa-banner-indicator"); if (details.style.display === "none") { details.style.display = "block"; indicator.textContent = "^"; } else { details.style.display = "none"; indicator.textContent = "v"; } } const monthName=new Array("January","February","March","April","May","June","July","August","September","October","November","December"); let currentDate = new Date(); let currentIsoDateStr = currentDate.toISOString().substring(0, 10); let currentDateStr = currentDate.getFullYear() + '-' + monthName[currentDate.getMonth()] + '-' + currentDate.getDate(); Data Access FTPS from SPDF (not with most browsers) HTTPS from SPDF CDAWeb WebService: CDAWeb Programmatic Data Access HAPI: CDAWeb HAPI Server ISEE 2 magnetometer 1-min data var authors='Russell, Christopher T.'; document.write(authors); (1987). ISEE 2 magnetometer 1-min data. [Data set]. University of California, Los Angeles; Space Physics Data Facility. https://doi.org/10.21978/p8t923. Accessed on document.write(currentDateStr);. Note: Proper references, including Copy BibTeX Citation or other formats, should include the "Accessed on date" to identify the version of the resource being cited in a given publication. 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. Metadata Rights CC0-1.0: Creative Commons Zero v1.0 Universal Note CC0 1.0 Universal is the Creative Commons license applicable to all publicly available SPASE metadata descriptions. The actual data/software may be subject to a different license. View XML | Edit Details Version:2.7.1 NumericalData ResourceID spase://NASA/NumericalData/ISEE2/MAG/PT1M NamingAuthority NASA ResourceType NumericalData ResourceHeader ResourceName ISEE 2 magnetometer 1-min data DOI https://doi.org/10.21978/p8t923 ReleaseDate 2026-06-26 13:18:07Z RevisionHistory RevisionEvent ReleaseDate 2021-05-31 12:34:56.789Z Note Updated to SPASE Version 2.3.2 if needed, Applied quality control for DOI usage, LFB RevisionEvent ReleaseDate 2025-09-30 14:25:28Z Note Updated PublishedBy name to match ROR Registry. Added ResourceType and NamingAuthority. Changed http to https in top-level schemaLocation attribute. Fixed version number separator in top-level schemaLocation attribute. Matched version number in schemaLocation attribute to updated value in Version tag. ZCB RevisionEvent ReleaseDate 2025-12-04 13:29:38Z Note Added MetadataRightsList and RightsList(s). Updated to 2.7.1. ZCB RevisionEvent ReleaseDate 2026-06-26 13:18:07Z Note Add 'Z' to RevisionEvent:ReleaseDate(s), PublicationDate, TemporalDescription:TimeSpan:StartDate, TemporalDescription:TimeSpan:StopDate. ZCB 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 00:00:00Z PublishedBy University of California, Los Angeles; Space Physics Data Facility Contacts Role Person StartDate StopDate Note 1. PrincipalInvestigator spase://SMWG/Person/Christopher.T.Russell 2. DataProducer spase://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 RightsList Rights SchemeURI https://spdx.org/licenses/ RightsIdentifierScheme SPDX RightsIdentifier CC0-1.0 RightsURI https://spdx.org/licenses/CC0-1.0.html RightsName Creative Commons Zero v1.0 Universal Note CC0 1.0 Universal is the Creative Commons license applicable to all publicly available NASA Heliophysics data products 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 RightsList Rights SchemeURI https://spdx.org/licenses/ RightsIdentifierScheme SPDX RightsIdentifier CC0-1.0 RightsURI https://spdx.org/licenses/CC0-1.0.html RightsName Creative Commons Zero v1.0 Universal Note CC0 1.0 Universal is the Creative Commons license applicable to all publicly available NASA Heliophysics data products 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 AccessDirectoryTemplate https://cdaweb.gsfc.nasa.gov/pub/data/isee/isee2/isee2_cdaweb/60sec_mfi/$Y AccessFilenameTemplate isee2_60sec_mfi_$Y$m$d_$v.cdf Acknowledgement UCLA ISEE Magnetometer and GSFC CDAWeb teams AccessInformation RepositoryID spase://SMWG/Repository/NASA/GSFC/SPDF Availability Online AccessRights Open AccessURL Name CDAWeb Programmatic Data Access URL https://cdaweb.gsfc.nasa.gov/WS/cdasr/1/dataviews/sp_phys/datasets/ISEE2_60SEC_MFI/clientLibraryExample/ Style WebService ProductKey ISEE2_60SEC_MFI Description Access to this data from common programming environments. Note: this AccessInformation element was added by HDPWS. Format Binary Acknowledgement UCLA ISEE Magnetometer and GSFC CDAWeb teams AccessInformation RepositoryID spase://SMWG/Repository/NASA/GSFC/SPDF Availability Online AccessRights Open RightsList Rights SchemeURI https://spdx.org/licenses/ RightsIdentifierScheme SPDX RightsIdentifier CC0-1.0 RightsURI https://spdx.org/licenses/CC0-1.0.html RightsName Creative Commons Zero v1.0 Universal Note CC0 1.0 Universal is the Creative Commons license applicable to all publicly available NASA Heliophysics data products 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 21:04:19Z StopDate 1987-09-26 16:10:30Z 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