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ISEE1 Resonance Sounder Orbital Parameters (CDF)

ResourceID
spase://CNES/NumericalData/CDPP-Archive/ISEE1/Ephemeris/ISEE1_SND_AUX

Description

This data set contains all orbital parameters from the ISEE1 SND resonance sounder instrument at the time of sounder operation - Distance, Velocity, Attitude... - in various reference frames and the observed magnetic field for each recorded spectra.

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Details

Version:2.4.0

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-Archive/ISEE1/Ephemeris/ISEE1_SND_AUX
ResourceHeader
ResourceName
ISEE1 Resonance Sounder Orbital Parameters (CDF)
DOI
https://doi.org/10.24400/802406/hkk1-vpmq
ReleaseDate
2022-02-04 16:22:02Z
Description

This data set contains all orbital parameters from the ISEE1 SND resonance sounder instrument at the time of sounder operation - Distance, Velocity, Attitude... - in various reference frames and the observed magnetic field for each recorded spectra.

Acknowledgement
We suggest contacting P. Canu (LPP) when using these data and for any further question. In publications, we recommend to add the following sentence in the acknowledgments: The authors acknowledge CNES (Centre National d'Etudes Spatiales) and CRPE (now LPP) for support for operations of the instrument and production of these data and CDPP for their archiving and provision.
Contacts
RolePersonStartDateStopDateNote
1.GeneralContactspase://CNES/Person/CDPP-Archive/Robert.McGuire
AccessInformation
RepositoryID
Availability
Online
AccessURL
Name
REGARDS
URL
Description

Access via CNES Data Archive for CDPP

Format
CDF
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1977-10-22 00:00:00Z
StopDate
1987-07-30 00:00:00Z
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Heliosphere.NearEarth
Parameter #1
Name
ISEE-1 Position (GSE frame)
Description

ISEE-1 Position relative to Earth in km (Cartesian GSE frame)

Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #2
Name
ISEE-1 Position (GEI frame)
Description

ISEE-1 Position relative to Earth in km (Cartesian GEI frame)

Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GEI
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #3
Name
ISEE-1 Position relative to Earth
Description

ISEE-1 Position relative to Earth in km (Cartesian GSM frame)

Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #4
Name
ISEE-1 Spacecraft Velocity (GSE)
Description

ISEE-1 Velocity (Cartesian GSE frame)

Units
km/s
UnitsConversion
1e3>m/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Velocity
Parameter #5
Name
ISEE-1 Angular Velocity (GSE)
Description

ISEE-1 Angular Velocity in rad/s (Cartesian GSE frame)

Units
rad/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Velocity
Parameter #6
Name
ISEE-1 Euler angles relative to GSE frame
Description

ISEE-1 Euler angles relative to GSE frame

Units
rad
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
SupportQuantity
Other