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Double Star 2 EPOS Catalogues Predicted Geometric Positions

ResourceID
spase://CNES/NumericalData/CDPP-Archive/DoubleStar2/EPOS/Catalogues/DSTAR_JP_T2_PGP

Description
This data set contains the predicted position and velocity of the Double Star 2 spacecraft, the GSE to GSM rotation angle and the dipole tilt, at five minute intervals. The data are provided by the European Payload Operations Service (EPOS).

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Details

Version:2.4.0

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-Archive/DoubleStar2/EPOS/Catalogues/DSTAR_JP_T2_PGP
ResourceHeader
ResourceName
Double Star 2 EPOS Catalogues Predicted Geometric Positions
DOI
https://doi.org/10.24400/802406/9yfe-cd29
ReleaseDate
2021-11-02 15:44:52Z
Description
This data set contains the predicted position and velocity of the Double Star 2 spacecraft, the GSE to GSM rotation angle and the dipole tilt, at five minute intervals. The data are provided by the European Payload Operations Service (EPOS).
Acknowledgement
Refer to www.epos.rl.ac.uk for rules of acknowledgement
Contacts
Role Person StartDate StopDate Note
1. PrincipalInvestigator spase://CNES/Person/CDPP-Archive/Michael.A.Hapgood
AccessInformation
RepositoryID
Availability
Online
AccessURL
Name
REGARDS
URL
Description
Access via CNES Data Archive for CDPP
Format
CDF
InstrumentIDs
MeasurementType
InstrumentStatus
TemporalDescription
TimeSpan
StartDate
2004-07-01 00:00:00Z
StopDate
2009-03-01 00:00:00Z
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosphere.Magnetotail
ObservedRegion
Earth.Magnetosphere.Main
ObservedRegion
Earth.Magnetosphere.RadiationBelt
ObservedRegion
Earth.NearSurface.Ionosphere
ObservedRegion
Earth.NearSurface.Plasmasphere
Parameter #1
Name
Status components
Description
Label for Status components
Support
SupportQuantity
Other
Parameter #2
Name
GSE cartesian components
Description
Components in GSE cartesian coordinates
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #3
Name
Half interval
Description
Half the mean separation between time tags, averaged over the file
Support
SupportQuantity
Other
Parameter #4
Name
Orbit number
Description
Orbit number including phase
Support
SupportQuantity
Other
Parameter #5
Name
Predicted Position of T2
Description
Predicted Position of ref T2
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #6
Name
Predicted Velocity of T2
Description
Predicted Velocity of ref T2
Units
km/s
UnitsConversion
1.0e3>m s^-1
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Velocity
Parameter #7
Name
Predicted gse Latitude of T2 axis
Description
Predicted gse Latitude of T12axis, Angle from Ecliptic Plane
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Positional
Parameter #8
Name
Predicted gse Longitude of T2 axis
Description
Predicted gse Longitude of T2 axis, Angle from x in x-y (GSE) plane
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Positional
Parameter #9
Name
Predicted Rotation angle GSE to GSM
Description
Predicted Rotation angle GSE to GSM, positive from +z towards +y
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Other
Parameter #10
Name
Predicted Dipole Tilt in GSM z-x Plane
Description
Predicted Dipole Tilt in GSM z-x Plane, positive from +z towards +x
Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Other