Version:2.4.1
NumericalData
ResourceID
spase://CNES/NumericalData/CDPP-AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all
ResourceHeader
ResourceName
Interball Tail - Ephemeris - orbit
ReleaseDate
2013-05-24 12:42:32Z
Description
Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags.
Acknowledgement
The Interball project, Russian Space Research Institute (IKI) and Dr. Prokhorenko
Contacts
InformationURL
Name
IKI Satellite Situation Center
URL
Description
This page maintains the Situation Analysis for the IKI International Space Missions and its coordination with the Inter-Agency multimission campaigns.
InformationURL
Name
Interball Tail Probe Situation Analysis
URL
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
Style
HAPI
ProductKey
intt-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
CDAWeb
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1995-08-04 00:01:00Z
StopDate
2000-10-16 13:55:00Z
Cadence
PT2M
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Earth.Magnetosphere.Main
ObservedRegion
Heliosphere.NearEarth
Caveats
The data cadence varies
Parameter #1
Name
xyz_gse
ParameterKey
it_xyz
Description
Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km)
UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
UnitsConversion
6.37e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
ValueFormat
F7.3
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
it_xyz(0)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
it_xyz(1)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
it_xyz(2)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #2
Name
xyz_gsm
ParameterKey
it_xyz_gsm
Description
Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km)
UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
UnitsConversion
6.37e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
RenderingHints
DisplayType
TimeSeries
ValueFormat
F7.3
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
it_xyz_gsm(0)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
it_xyz_gsm(1)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
it_xyz_gsm(2)
ValidMin
-30.0
ValidMax
30.0
FillValue
-1.0E31
Support
Qualifier
Vector
SupportQuantity
Positional