Version:2.4.1
NumericalData
ResourceID
spase://CNES/NumericalData/CDPP-AMDA/Cluster/Cluster4/Ephemeris/clust4-orb-all
ResourceHeader
ResourceName
Cluster 4 - Ephemeris - orbit
ReleaseDate
2024-09-30 08:34:53Z
Description
Cluster-4 position
Contacts
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
Style
HAPI
ProductKey
clust4-orb-all
Description
Web Service to this product using the HAPI interface.
Format
CSV
Acknowledgement
Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA Web application
URL
Description
Access to Data via CDPP/AMDA Web application.
Format
CSV
Format
VOTable
Format
CDF
Format
PNG
Acknowledgement
Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers.
ProviderName
IRAP
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
2000-08-22 00:00:00Z
StopDate
2024-09-20 23:14:00Z
Cadence
PT1M
Parameter #1
Name
xyz_gse
ParameterKey
c4_xyz_gse
Description
Spacecraft position in GSE
UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
UnitsConversion
6.4e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
c4_xyz_gse(0)
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
c4_xyz_gse(1)
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
c4_xyz_gse(2)
FillValue
-1.0E31
Support
SupportQuantity
Positional
Parameter #2
Name
xyz_gsm
ParameterKey
c4_xyz_gsm
Description
Spacecraft position in GSM
UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
UnitsConversion
6.4e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
c4_xyz_gsm(0)
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
c4_xyz_gsm(1)
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
c4_xyz_gsm(2)
FillValue
-1.0E31
Support
SupportQuantity
Positional
Parameter #3
Name
distance c4-earth
ParameterKey
c4_r
UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
RenderingHints
ValidMin
0.0
FillValue
-1.0E31
Support
Qualifier
Magnitude
SupportQuantity
Positional