Version:2.4.1
NumericalData
ResourceID
spase://CNES/NumericalData/CDPP-AMDA/UKS/ORBIT/uks-orb-all
ResourceHeader
ResourceName
AMPTE - UKS - Ephemeris - orbit
AlternateName
ephemeris
ReleaseDate
2020-02-04 16:16:40Z
Description
Acknowledgement
User will acknowledge the AMPTE/UKS team in any publication resulting from the use of these data.
Contacts
InformationURL
Name
NSSDC Master Catalog
URL
Description
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
Style
HAPI
ProductKey
uks-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.
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1984-08-18 23:55:00Z
StopDate
1985-01-15 08:00:00Z
Cadence
PT300S
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosphere.Magnetotail
ObservedRegion
Heliosphere.NearEarth
Parameter #1
Name
xyz_gse
ParameterKey
uks_orb_xyz
Description
Spacecraft position in GSE Cartesian coordinates
Units
Re
UnitsConversion
6.378e6;km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
uks_orb_xyz(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
uks_orb_xyz(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
uks_orb_xyz(2)
Support
SupportQuantity
Positional
Parameter #2
Name
xyz_gsm
ParameterKey
uks_orb_gsm
Description
Spacecraft position in GSM Cartesian coordinates
Units
Re
UnitsConversion
6.378e6;km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
RenderingHints
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
uks_orb_gsm(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
uks_orb_gsm(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
uks_orb_gsm(2)
Support
SupportQuantity
Positional
Parameter #3
Name
IRM_to_UKS_gse
ParameterKey
uks_orb_scdist
Description
UKS Spacecraft position relative to IRM in GSE Cartesian coordinates
Units
km
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
uks_orb_scdist(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
uks_orb_scdist(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
uks_orb_scdist(2)
Support
SupportQuantity
Positional
Parameter #4
Name
vel_gse
ParameterKey
uks_orb_v
Description
Spacecraft velocity in GSE Cartesian coordinates
Units
km/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
Structure
Size
3
Element
Name
vx
Qualifier
Component.I
Index
1
ParameterKey
uks_orb_v(0)
Element
Name
vy
Qualifier
Component.J
Index
2
ParameterKey
uks_orb_v(1)
Element
Name
vz
Qualifier
Component.K
Index
3
ParameterKey
uks_orb_v(2)
Support
SupportQuantity
Positional
Parameter #5
Name
vel_gsm
ParameterKey
uks_orb_vgsm
Description
Spacecraft velocity in GSM Cartesian coordinates
Units
km/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
RenderingHints
Structure
Size
3
Element
Name
vx
Qualifier
Component.I
Index
1
ParameterKey
uks_orb_vgsm(0)
Element
Name
vy
Qualifier
Component.J
Index
2
ParameterKey
uks_orb_vgsm(1)
Element
Name
vz
Qualifier
Component.K
Index
3
ParameterKey
uks_orb_vgsm(2)
Support
SupportQuantity
Positional
Parameter #6
Name
distance uks-earth
ParameterKey
uks_orb_mag
Description
Spacecraft distance to earth center
Units
Re
RenderingHints
Support
SupportQuantity
Positional