Version:2.4.1
NumericalData
ResourceID
spase://CNES/NumericalData/CDPP-AMDA/MMS/MMS3/Ephemeris/mms3-orb-t89d
ResourceHeader
ResourceName
MMS3 - Ephemeris - orbit t89d
ReleaseDate
2024-05-23 02:41:27Z
Description
MMS3 position
Contacts
InformationURL
Name
MMS homepage at GSFC
URL
InformationURL
Name
Science Data Center at LASP
URL
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDPP/AMDA HAPI Server
URL
Style
HAPI
ProductKey
mms3-orb-t89d
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
LANL
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
2015-03-13 00:00:00Z
StopDate
2024-04-29 23:59:30Z
Cadence
PT30S
Parameter #1
Name
xyz_gse
ParameterKey
mms3_xyz_gse
Description
Spacecraft position in GSE
UCD
pos.earth;instr.obsty
Units
Re
UnitsConversion
6.4e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
mms3_xyz_gse(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
mms3_xyz_gse(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
mms3_xyz_gse(2)
Support
SupportQuantity
Positional
Parameter #2
Name
xyz_gsm
ParameterKey
mms3_xyz_gsm
Description
Spacecraft position in GSM
UCD
pos.earth;instr.obsty
Units
Re
UnitsConversion
6.4e6>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSM
RenderingHints
Structure
Size
3
Element
Name
x
Qualifier
Component.I
Index
1
ParameterKey
mms3_xyz_gsm(0)
Element
Name
y
Qualifier
Component.J
Index
2
ParameterKey
mms3_xyz_gsm(1)
Element
Name
z
Qualifier
Component.K
Index
3
ParameterKey
mms3_xyz_gsm(2)
Support
SupportQuantity
Positional
Parameter #3
Name
distance mms3-earth
ParameterKey
mms3_r
UCD
pos.distance;instr.obsty
Units
Re
RenderingHints
ValidMin
0.0
FillValue
-1.0E31
Support
Qualifier
Magnitude
SupportQuantity
Positional