Version:2.6.0
NumericalData
ResourceID
spase://NOAA/NumericalData/DSCOVR/Ephemeris/Orbit/Preliminary/PT1M
ResourceHeader
ResourceName
DSCOVR Orbital Ephemeris Predicted Spacecraft Position and Velocity
ReleaseDate
2024-06-20 12:34:56.789
RevisionHistory
RevisionEvent
ReleaseDate
2021-04-27 17:52:57
Note
Only known prior ReleaseDate of the metadata
RevisionEvent
ReleaseDate
2024-06-20 12:34:56.789
Note
Replaced StopDate with a RelativeStopDate equal to P1M, SPASE versioned up to 2.6.0, LFB 20240620
Description
DSCOVR Predicted Orbit Data File
Acknowledgement
A. Szabo
Contacts
InformationURL
Name
Deep Space Climate Observatory, DSCOVR, Web Page, NESDIS, NOAA
URL
Description
Deep Space Climate Observatory, DSCOVR, Web Page hosted by the National Environmental Satellite, Data, and Information Service, NESDIS, National Oceanic and Atmospheric Administration, NOAA
PriorIDs
spase://VSPO/NumericalData/DSCOVR/Ephemeris/Orbit/PT1M
spase://VSPO/NumericalData/DSCOVR/Ephemeris/Orbit/Preliminary/PT1M
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description
In CDF via ftp from SPDF.
AccessURL
Name
HTTPS from SPDF
URL
Description
In CDF via http from SPDF.
AccessURL
Name
CDAWeb
URL
ProductKey
DSCOVR_ORBIT_PRE
Description
Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb
Format
CDF
Encoding
None
Acknowledgement
A. Szabo. Please acknowledge the data providers and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
DSCOVR_ORBIT_PRE
Description
Web Service to this product using the HAPI interface.
Format
CSV
Acknowledgement
A. Szabo. Please acknowledge the data providers and CDAWeb when using these data.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
2015-02-11 00:00:00.000
RelativeStopDate
P1M
Cadence
PT10S
ObservedRegion
Heliosphere
ObservedRegion
Heliosphere.NearEarth
ObservedRegion
Heliosphere.Inner
Parameter #1
Name
Epoch Time, since 0 A.D.
ParameterKey
Epoch
Description
Epoch Time, Milliseconds since 0 A.D.
Caveats
This parameter exhibits an increasing monotonic progression.
Cadence
PT10S
Units
ms
UnitsConversion
1e-3>s
RenderingHints
AxisLabel
Epoch
ValueFormat
E14.8
ValidMin
11-Feb-2015 00:00:00.000
ValidMax
11-Feb-2065 00:00:00.000
FillValue
31-Dec-9999 23:59:59.999
Support
Parameter #2
Name
Time PB5
Set
Time series defined by using: EPOCH
ParameterKey
Time_PB5
Description
Time in PB5 Format: Year, Day, Milliseconds, Observation Time
Cadence
PT10S
Structure
Size
3
Element
Name
Year
Index
1
Units
year
ValidMin
2015
ValidMax
2065
Element
Name
Day of Year
Index
2
Units
d
ValidMin
0
ValidMax
366
Element
Name
Elapsed milliseconds of day
Index
3
Units
ms
ValidMin
0
ValidMax
86400000
FillValue
-2147483647
Support
Parameter #3
Name
Sun-Earth Radial Distance
Set
Time series defined by using: EPOCH
ParameterKey
SUN_R
Description
Sun-Earth Radial Distance
Cadence
PT10S
Units
km
UnitsConversion
1e3>m
RenderingHints
DisplayType
TimeSeries
AxisLabel
Earth Distance from Sun
ValueFormat
F17.5
ScaleMin
1.45e+08
ScaleMax
1.55e+08
ValidMin
0.0
ValidMax
1.8e+08
FillValue
-1.0e+31
Support
Qualifier
Magnitude
SupportQuantity
Positional
Parameter #4
Name
Spacecraft Position, J2000 GCI
Set
Time series defined by using: EPOCH
ParameterKey
GCI_POS
Description
Spacecraft Position Vector, Geocentric Inertial, J2000 GCI, Cartesian Coordinates
Cadence
PT10S
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GEI
RenderingHints
DisplayType
TimeSeries
ValueFormat
F17.5
ScaleMin
-1.8e+06
ScaleMax
1.8e+06
Structure
Size
3
Element
Element
Element
ValidMin
-1.8e+06
ValidMax
1.8e+06
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #5
Name
Spacecraft Velocity, J2000 GCI
Set
Time series defined by using: EPOCH
ParameterKey
GCI_VEL
Description
Spacecraft Velocity Vector, Geocentric Inertial, J2000 GCI, Cartesian Coordinates
Cadence
PT10S
Units
km/s
UnitsConversion
1e3>m/s
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GEO
RenderingHints
DisplayType
TimeSeries
ValueFormat
F12.7
ScaleMin
-12.0
ScaleMax
12.0
Structure
Size
3
Element
Element
Element
ValidMin
-12.0
ValidMax
12.0
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #6
Name
Spacecraft Position, GSE
Set
Time series defined by using: EPOCH
ParameterKey
GSE_POS
Description
Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE Cartesian Coordinates
Cadence
PT10S
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
ValueFormat
F17.5
ScaleMin
-1.8e+06
ScaleMax
1.8e+06
Structure
Size
3
Element
Element
Element
ValidMin
-1.8e+06
ValidMax
1.8e+06
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional
Parameter #7
Name
Moon Position, GSE
Set
Time series defined by using: EPOCH
ParameterKey
MOON_GSE_POS
Description
Moon Position Vector, Geocentric Solar Ecliptic, GSE Cartesian Coordinates
Cadence
PT10S
Units
km
UnitsConversion
1e3>m
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
ValueFormat
F17.5
ScaleMin
-450000.0
ScaleMax
450000.0
Structure
Size
3
Element
Element
Element
ValidMin
-1.8e+06
ValidMax
1.8e+06
FillValue
-1.0e+31
Support
Qualifier
Vector
SupportQuantity
Positional