HPDE.io

Data Access

ACE - Ephemeris - orbit L1

ResourceID
spase://CNES/NumericalData/CDPP-AMDA/ACE/Ephemeris/ace-orb-all

Description

ACE orbits the L1 libration point which is a point of Earth-Sun gravitational equilibrium about 1.5 million km from
Earth and 148.5 million km from the Sun

View XML | View JSON | Edit

Details

Version:2.4.1

NumericalData

ResourceID
spase://CNES/NumericalData/CDPP-AMDA/ACE/Ephemeris/ace-orb-all
ResourceHeader
ResourceName
ACE - Ephemeris - orbit L1
AlternateName
orbit L1 libration point
ReleaseDate
2024-09-30 06:44:30Z
Description

ACE orbits the L1 libration point which is a point of Earth-Sun gravitational equilibrium about 1.5 million km from
Earth and 148.5 million km from the Sun

Contacts
RolePersonStartDateStopDateNote
1.TechnicalContactspase://CNES/Person/CDPP-AMDA/Benjamin.Renard
AccessInformation
RepositoryID
spase://SMWG/Repository/CDPP/AMDA
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
https://amda.irap.omp.eu/service/hapi
Style
HAPI
ProductKey
ace-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
spase://SMWG/Repository/CDPP/AMDA
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA Web application
URL
https://amda.cdpp.eu
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/SSCWeb
InstrumentIDs
spase://CNES/Instrument/CDPP-AMDA/ACE/Ephemeris
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1997-08-25 17:48:00Z
StopDate
2024-09-30 23:59:00Z
Cadence
PT12M
Parameter #1
Name
xyz_gse
ParameterKey
ace_xyz_gse
Description

Spacecraft position in GSE

UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
ace_xyz_gse(0)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
ace_xyz_gse(1)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
ace_xyz_gse(2)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Support
SupportQuantity
Positional
Parameter #2
Name
xyz_gsm
ParameterKey
ace_xyz_gsm
Description

Spacecraft position in GSM

UCD
pos.ephem;pos.earth;instr.obsty
Units
Re
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
ace_xyz_gsm(0)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
ace_xyz_gsm(1)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
ace_xyz_gsm(2)
ValidMin
-1594535.0
ValidMax
1594535.0
FillValue
-1.0E31
Support
SupportQuantity
Positional
Parameter #3
Name
xyz_hci
ParameterKey
ace_xyz_hci
Description

Spacecraft position in HCI

UCD
pos.ephem;pos.earth;instr.obsty
Units
AU
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
HCI
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
ace_xyz_hci(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
ace_xyz_hci(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
ace_xyz_hci(2)
Support
SupportQuantity
Positional
Parameter #4
Name
xyz_hee
ParameterKey
ace_xyz_hee
Description

Spacecraft position in HEE

UCD
pos.ephem;pos.earth;instr.obsty
Units
AU
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
HEE
RenderingHints
DisplayType
TimeSeries
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
ace_xyz_hee(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
ace_xyz_hee(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
ace_xyz_hee(2)
Support
SupportQuantity
Positional
Parameter #5
Name
distance ace-earth
ParameterKey
ace_r
UCD
pos.distance
Units
Re
Support
SupportQuantity
Positional
Parameter #6
Name
distance ace-sun
ParameterKey
ace_r_sun
UCD
pos.distance
Units
AU
Support
SupportQuantity
Positional
Parameter #7
Name
lon hee
ParameterKey
ace_lon_hee
UCD
pos.bodyrc.lon
Units
deg
RenderingHints
DisplayType
TimeSeries
Support
SupportQuantity
Positional
Parameter #8
Name
lat hee
ParameterKey
ace_lat_hee
UCD
pos.bodyrc.lat
Units
deg
RenderingHints
DisplayType
TimeSeries
Support
SupportQuantity
Positional