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Double Star 1 EPOS Catalogues Predicted Geometric Positions

ResourceID
spase://CNES/NumericalData/CDPP-Archive/DoubleStar1/EPOS/Catalogues/DSTAR_JP_T1_PGP

Description

This data set contains the predicted position and velocity of the Double Star 1 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/DoubleStar1/EPOS/Catalogues/DSTAR_JP_T1_PGP
ResourceHeader
ResourceName
Double Star 1 EPOS Catalogues Predicted Geometric Positions
DOI
https://doi.org/10.24400/802406/nx2e-r7sa
ReleaseDate
2021-11-02 15:44:52Z
Description

This data set contains the predicted position and velocity of the Double Star 1 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
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://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
2004-01-01 00:00:00Z
StopDate
2007-10-01 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 T1
Description

Predicted Position of ref T1

Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #6
Name
Predicted Velocity of T1
Description

Predicted Velocity of ref T1

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 T1 axis
Description

Predicted gse Latitude of T1 axis, Angle from Ecliptic Plane

Units
°
UnitsConversion
0.0174532925>rad
Support
SupportQuantity
Positional
Parameter #8
Name
Predicted gse Longitude of T1 axis
Description

Predicted gse Longitude of T1 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