HPDE.io

Cluster Predicted Geometric Positions (PGP) Spacecraft Tetrahedron, JSOC Parameter (JP), 5 min Data

ResourceID
spase://ESA/NumericalData/Cluster/Ephemeris/JP/PredictedGeometricPosition/PT5M

Description

Cluster Predicted Geometric Positions generated by the Joint Science Operations Centre, JSOC. See M.A. Hapgood et al., The Joint Science Operations Centre, Space Sci. Rev., 79, 487-525, 1997.
For Geometrical Configuration Parameters, see page 328 of Tetrahedron Geometric Factors by P. Robert et al., in Analysis Methods for Multi-Spacecraft Data, Editors G. Paschmann and P. Daly, published in 1998 by the European Space Agency, ESA, and the International Space Science Institute, ISSI, Bern.

View XML | View JSON | Edit

Details

Version:2.3.0

NumericalData

ResourceID
spase://ESA/NumericalData/Cluster/Ephemeris/JP/PredictedGeometricPosition/PT5M
ResourceHeader
ResourceName
Cluster Predicted Geometric Positions (PGP) Spacecraft Tetrahedron, JSOC Parameter (JP), 5 min Data
ReleaseDate
2021-04-27 17:52:14Z
Description

Cluster Predicted Geometric Positions generated by the Joint Science Operations Centre, JSOC. See M.A. Hapgood et al., The Joint Science Operations Centre, Space Sci. Rev., 79, 487-525, 1997.
For Geometrical Configuration Parameters, see page 328 of Tetrahedron Geometric Factors by P. Robert et al., in Analysis Methods for Multi-Spacecraft Data, Editors G. Paschmann and P. Daly, published in 1998 by the European Space Agency, ESA, and the International Space Science Institute, ISSI, Bern.

Acknowledgement
M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement
Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Michael.A.Hapgood
2.MetadataContactspase://SMWG/Person/Robert.E.McGuire
3.MetadataContactspase://SMWG/Person/Lee.Frost.Bargatze
InformationURL
Name
Cluster Science Archive, CSA, Web Page
URL
Description

Web Page for access to High-Time Resolution Data from the Cluster and Double Star Missions

InformationURL
Name
Cluster Science Data System, CSDS, Web Page
URL
Description

The Cluster Science Working Team along with the ESA Cluster Project Team have established the Cluster Science Data System, CSDS, a distributed Set of Data Centres, most of which are associated with one or more of the Cluster Experiments. With Software provided by the Experiment Team, each Data Centre processes the Data and then exchanges them with all the other Centres to obtain a full Data Set in a standard Format.

PriorIDs
spase://ESA/NumericalData/Cluster/Ephemeris/JP/PGP/PT1M
spase://VSPO/NumericalData/P_CLUSTER1_HDR_PGP_60S
spase://VSPO/NumericalData/Cluster/Ephemeris/JP-PGP/PT1M
spase://VSPO/NumericalData/Cluster/Ephemeris/JP/PGP/PT1M
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description

Access to Data in CDF Format via ftp from SPDF

AccessURL
Name
HTTPS from SPDF
URL
Description

Access to Data in CDF Format via http from SPDF

AccessURL
Name
CDAWeb
URL
ProductKey
CL_JP_PGP
Description

Access to ASCII, CDF, and Plots via NASA/GSFC CDAWeb

Format
CDF
Encoding
None
Acknowledgement
M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement. Please acknowledge the Data Providers and CDAWeb when using these Data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
CL_JP_PGP
Description

Web Service to this product using the HAPI interface.

Format
CSV
Acknowledgement
M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement. Please acknowledge the Data Providers and CDAWeb when using these Data.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
Ephemeris
MeasurementType
InstrumentStatus
TemporalDescription
TimeSpan
StartDate
2000-08-14 20:35:00.000
RelativeStopDate
P3Y
Cadence
PT5M
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosphere.Magnetotail
ObservedRegion
Earth.Magnetosphere.Main
ObservedRegion
Earth.Magnetosphere.RadiationBelt
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Heliosphere.NearEarth
Caveats
JSOC Predicted Orbits, calculated by using Cluster-Samba, C3, as the Reference Spacecraft
Parameter #1
Name
Half Interval
ParameterKey
Half_interval__CL_JP_PGP
Description

Half Interval, equal to Half of the Separation between Time Tags averaged of the over the File

Cadence
PT5M
Units
ms
UnitsConversion
1.0e-3>s
RenderingHints
AxisLabel
Half Sample Time Interval
FillValue
-1.0e+31
Support
SupportQuantity
Temporal
Parameter #2
Name
Epoch Time Tags
ParameterKey
Epoch__CL_JP_PGP
Description

Epoch Time Tags, Spot Value Time Tags

Caveats
This Parameter exhibits an increasing Monotonic Progression.
Cadence
PT5M
Units
ms
UnitsConversion
1.0e-3>s
RenderingHints
AxisLabel
Epoch
ScaleMin
6.3145505019904e+13
ScaleMax
6.3148183419904e+13
ScaleType
LinearScale
ValidMin
01-Jan-1994 00:00:00.000
ValidMax
01-Jan-2010 00:00:00.000
FillValue
-1.0e+31
Support
SupportQuantity
Temporal
Parameter #3
Name
Spacecraft Orbit Number, including Phase
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_orbit_num__CL_JP_PGP
Description

Spacecraft Orbit Number, including Fractional Phase Part

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1.0>(orbit.phase)
RenderingHints
AxisLabel
Fract Orbit
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
500.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
1000.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #4
Name
Predicted Spacecraft Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, for the Reference Satellite
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_r_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, for the Reference Satellite

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-150000.0
ScaleMax
150000.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
x (GSE) pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
y (GSE) pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
z (GSE) pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-140000.0
ValidMax
140000.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #5
Name
Predicted Spacecraft Velocity Vector, Geocentric Solar Ecliptic Cartesian Coordinates, for the Reference Satellite
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_v_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft Velocity Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, for the Reference Satellite

Caveats
Average Type: standard
Cadence
PT5M
Units
km/s
UnitsConversion
1.0e3>m/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-10.0
ScaleMax
10.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
Vx (GSE) pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
Vy (GSE) pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
Vz (GSE) pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-10.0
ValidMax
10.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #6
Name
Predicted Spacecraft 1, Cluster-Rumba, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr1_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft 1, Cluster-Rumba, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-20000.0
ScaleMax
20000.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
C1 dx pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
C1 dy pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
C1 dz pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-100000.0
ValidMax
100000.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #7
Name
Predicted Spacecraft 2, Cluster-Salsa, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr2_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft 2, Cluster-Salsa, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-20000.0
ScaleMax
20000.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
C2 dx pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
C2 dy pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
C2 dz pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-100000.0
ValidMax
100000.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #8
Name
Predicted Spacecraft 3, Cluster-Samba, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr3_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft 3, Cluster-Samba, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-20000.0
ScaleMax
20000.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
C3 dx pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
C3 dy pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
C3 dz pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-100000.0
ValidMax
100000.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #9
Name
Predicted Spacecraft 4, Cluster-Tango, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr4_xyz_gse__CL_JP_PGP
Description

Predicted Spacecraft 4, Cluster-Tango, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-20000.0
ScaleMax
20000.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
C4 dx pred
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
C4 dy pred
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
C4 dz pred
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-100000.0
ValidMax
100000.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #10
Name
Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at1_lat__CL_JP_PGP
Description

Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C1 Predicted Lat (GSE)
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-90.0
ValidMax
90.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.ElevationAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #11
Name
Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at1_long__CL_JP_PGP
Description

Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C1 Predicted Long (GSE)
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
360.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
360.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #12
Name
Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at2_lat__CL_JP_PGP
Description

Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C2 Predicted Lat (GSE)
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-90.0
ValidMax
90.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.ElevationAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #13
Name
Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at2_long__CL_JP_PGP
Description

Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C2 Predicted Long (GSE)
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
360.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
360.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #14
Name
Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at3_lat__CL_JP_PGP
Description

Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C3 Predicted Lat (GSE)
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-90.0
ValidMax
90.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.ElevationAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #15
Name
Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at3_long__CL_JP_PGP
Description

Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C3 Predicted Long (GSE)
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
360.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
360.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #16
Name
Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at4_lat__CL_JP_PGP
Description

Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C4 Predicted Lat (GSE)
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-90.0
ValidMax
90.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.ElevationAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #17
Name
Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_at4_long__CL_JP_PGP
Description

Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
C4 Predicted Long (GSE)
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
360.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
360.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #18
Name
Predicted Spacecraft Tetrahedron Shape Quality Parameter G
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_config_QG__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Shape Quality Parameter G, G=(Tetrahedron Volume/Ideal Volume)+(Tetrahedron Surface/Ideal Surface)+1

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1>(G_qual)
RenderingHints
AxisLabel
Q_G
ValueFormat
E13.6
ScaleMin
1.0
ScaleMax
3.0
ScaleType
LinearScale
ValidMin
1.0
ValidMax
3.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #19
Name
Predicted Spacecraft Tetrahedron Shape Quality Parameter, R
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_config_QR__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Shape Quality Parameter, R, R=norm*(Tetrahedron Volume/Sphere Volume)^1/3

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1>(R_qual)
RenderingHints
AxisLabel
Q_R
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
1.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
1.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #20
Name
Predicted Spacecraft Separation Minimum Distance
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr_min__CL_JP_PGP
Description

Predicted Spacecraft Separation Minimum Distance

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
RenderingHints
AxisLabel
Predicted Sep Min
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
20000.0
ScaleType
LogScale
ValidMin
0.0
ValidMax
1.0e+07
FillValue
-1.0e+31
Support
Qualifier
Magnitude
Qualifier
Scalar
SupportQuantity
Positional
Parameter #21
Name
Predicted Spacecraft Separation Maximum Distance
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_dr_max__CL_JP_PGP
Description

Predicted Spacecraft Separation Maximum Distance

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
RenderingHints
AxisLabel
Predicted Sep Max
ValueFormat
E13.6
ScaleMin
1.0
ScaleMax
20000.0
ScaleType
LogScale
ValidMin
0.0
ValidMax
1.0e+07
FillValue
-1.0e+31
Support
Qualifier
Magnitude
Qualifier
Scalar
SupportQuantity
Positional
Parameter #22
Name
Predicted Coordinate System Rotation Angle, Geocentric Solar Ecliptic to Geocentric Solar Magnetospheric
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
gse_gsm__CL_JP_PGP
Description

Predicted Coordinate System Rotation Angle, Geocentric Solar Ecliptic, GSE, to Geocentric Solar Magnetospheric, GSM

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
Predicted GSE GSM
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-40.0
ValidMax
40.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #23
Name
Predicted Magnetic Dipole Tilt Angle in the Geocentric Solar Magnetosphreric X-Z Plane
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
dipole_tilt__CL_JP_PGP
Description

Predicted Magnetic Dipole Tilt Angle in the Geocentric Solar Magnetosphreric, GSM, X-Z Plane

Caveats
Average Type: angle_degrees
Cadence
PT5M
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
AxisLabel
Predicted Pole Tilt
ValueFormat
E13.6
ScaleMin
-90.0
ScaleMax
90.0
ScaleType
LinearScale
ValidMin
-40.0
ValidMax
40.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Scalar
SupportQuantity
Positional
Parameter #24
Name
Predicted Spacecraft Tetrahedron Size Parameter, L
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_geom_size__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Size Parameter, L, Characteristic Size

Caveats
Average Type: standard
Cadence
PT5M
Units
km
UnitsConversion
1.0e3>m
RenderingHints
AxisLabel
Predicted Tetra L
ValueFormat
E13.6
ScaleMin
1.0
ScaleMax
100000.0
ScaleType
LogScale
ValidMin
0.0
ValidMax
1.0e+07
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #25
Name
Predicted Spacecraft Tetrahedron Elongation Parameter, E
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_geom_elong__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Elongation Parameter, E

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1>(Elongation)
RenderingHints
AxisLabel
Predicted Tetra E
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
1.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
1.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #26
Name
Predicted Spacecraft Tetrahedron Planarity Parameter, P
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_geom_planarity__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Planarity Parameter, P

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1>(Planarity)
RenderingHints
AxisLabel
Predicted Tetra P
ValueFormat
E13.6
ScaleMin
0.0
ScaleMax
1.0
ScaleType
LinearScale
ValidMin
0.0
ValidMax
1.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #27
Name
Predicted Spacecraft Tetrahedron Elongation Direction
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_geom_E_dir_gse__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Elongation Direction, expressed as Direction Cosines

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1.0>(direction)
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-1.0
ScaleMax
1.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
Dir_elongation_x (GSE)
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
Dir_elongation_y (GSE)
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
Dir_elongation_z (GSE)
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-1.0
ValidMax
1.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #28
Name
Predicted Spacecraft Tetrahedron Planarity Normal Direction
Set
Time Series defined by using: EPOCH__CL_JP_PGP
ParameterKey
sc_geom_P_nor_gse__CL_JP_PGP
Description

Predicted Spacecraft Tetrahedron Planarity Normal Direction, expressed as Direction Cosines

Caveats
Average Type: standard
Cadence
PT5M
UnitsConversion
1.0>(direction)
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
ValueFormat
E13.6
ScaleMin
-1.0
ScaleMax
1.0
ScaleType
LinearScale
Structure
Size
3
Element
Name
Nor_planarity_x (GSE)
Index
1
RenderingHints
AxisLabel
x (GSE)
Element
Name
Nor_planarity_y (GSE)
Index
2
RenderingHints
AxisLabel
y (GSE)
Element
Name
Nor_planarity_z (GSE)
Index
3
RenderingHints
AxisLabel
z (GSE)
ValidMin
-1.0
ValidMax
1.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional