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SOHO Definitive Attitude, 10 min Data, Satellite Body Axis Pitch, Roll, and Yaw Angles in GCI, GSE, GSM, and HEC Coordinates

ResourceID
spase://NASA/NumericalData/SOHO/Attitude/Definitive/PT10M

Description

SOHO 3-Axis Stabilized Definitive Attitude Data, Satellite Body Axis Orientation as specified by Pitch, Roll, and Yaw Angles in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, Geocentric Solar Magnetospheric, GSM, and Heliospheric Ecliptic, HEC, Coordinates

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Details

Version:2.3.2

NumericalData

ResourceID
spase://NASA/NumericalData/SOHO/Attitude/Definitive/PT10M
ResourceHeader
ResourceName
SOHO Definitive Attitude, 10 min Data, Satellite Body Axis Pitch, Roll, and Yaw Angles in GCI, GSE, GSM, and HEC Coordinates
ReleaseDate
2021-04-27 15:38:11Z
Description

SOHO 3-Axis Stabilized Definitive Attitude Data, Satellite Body Axis Orientation as specified by Pitch, Roll, and Yaw Angles in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, Geocentric Solar Magnetospheric, GSM, and Heliospheric Ecliptic, HEC, Coordinates

Contacts
RolePerson
1.ProjectScientistspase://SMWG/Person/Joseph.B.Gurman
2.MetadataContactspase://SMWG/Person/Robert.E.McGuire
3.MetadataContactspase://SMWG/Person/Lee.Frost.Bargatze
InformationURL
Name
SOHO Satellite Attitude and Orbit Information Website
URL
Description

SOHO Satellite Attitude and Orbit Information Website

InformationURL
Name
Satellite Situation Center, SSCWeb, System and Services
URL
Description

The Satellite Situation Center Web, SSCWeb, Service has been developed and is operated jointly by the NASA/GSFC Space Physics Data Facility, SPDF, and the National Space Science Data Center, NSSDC, to support a Range of NASA Science Programs and to fulfill Key International NASA Responsibilities including those of NSSDC and the World Data Center-A for Rockets and Satellites. The Software and associated Database of SSCWeb together form a System to cast Geocentric Spacecraft Location Information into a Framework of Empirical Geophysical Regions and Mappings of Spacecraft Locations along Lines of the Earth's Magnetic Field. This Capability is one Key to Mission Science Planning, both Single Missions and Coordinated Observations of Multiple Spacecraft with Ground-Based Investigations, and to subsequent Multi-Mission Data Analysis.

PriorIDs
spase://VSPO/NumericalData/SOHO/Attitude/Definitive/PT10M
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description

Access to Data in CDF Format via ftp from SPDF

AccessURL
Name
HTTPS from SPDF
URL
Description

Access to Data in CDF Format via http from SPDF

AccessURL
Name
CDAWeb
URL
ProductKey
SO_AT_DEF
Description

Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb

Format
CDF
Encoding
None
Acknowledgement
. 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
SO_AT_DEF
Description

Web Service to this product using the HAPI interface.

Format
CSV
Acknowledgement
. Please acknowledge the data providers and CDAWeb when using these data.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1995-05-22 00:05:00
StopDate
2002-09-22 23:55:00
Cadence
PT10M
ObservedRegion
Heliosphere
ObservedRegion
Heliosphere.NearEarth
ObservedRegion
Heliosphere.Inner
Parameter #1
Name
Epoch Time, SOHO Attitude
ParameterKey
Epoch
Description

Epoch Time, SOHO Attitude

Caveats
This parameter exhibits an increasing monotonic progression.
Cadence
PT10M
Units
ms
UnitsConversion
1e-3>s
RenderingHints
AxisLabel
Epoch
ScaleMin
6.2877146619904e+13
ScaleMax
6.3776657018904e+13
ValidMin
01-Jul-1992 00:00:00.000
ValidMax
31-Dec-2020 23:59:59.000
FillValue
-1.0e+31
Support
SupportQuantity
Temporal
Parameter #2
Name
Time PB5, Attitude
Set
Time series defined by using: EPOCH
ParameterKey
Time_PB5
Description

Time in PB5 Format: Year, Day, Milliseconds

Cadence
PT10M
Structure
Size
3
Element
Name
Year
Index
1
Units
year
ValidMin
1992
ValidMax
2020
RenderingHints
AxisLabel
year
ScaleMin
1992
ScaleMax
2020
Element
Name
Day of Year (Jan 1 = day 1)
Index
2
Units
d
ValidMin
183
ValidMax
366
RenderingHints
AxisLabel
day
ScaleMin
183
ScaleMax
366
Element
Name
Elapsed ms of Day
Index
3
Units
ms
ValidMin
0
ValidMax
86399000
RenderingHints
AxisLabel
msec
ScaleMin
0
ScaleMax
86399000
FillValue
-2147483648
Support
SupportQuantity
Temporal
Parameter #3
Name
Spacecraft Body Axis, Pitch Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_PITCH_AVG
Description

Spacecraft Body Axis, Pitch Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat p avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #4
Name
Spacecraft Body Axis, Roll Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_ROLL_AVG
Description

Spacecraft Body Axis, Roll Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat r avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #5
Name
Spacecraft Body Axis, Yaw Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_YAW_AVG
Description

Spacecraft Body Axis, Yaw Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat y avg
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #6
Name
Solar Axis Reference, Pitch Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAR_PITCH_AVG
Description

Solar Axis Reference, Pitch Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sar p avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #7
Name
Solar Axis Reference, Roll Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAR_ROLL_AVG
Description

Solar Axis Reference, Roll Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sar r avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #8
Name
Solar Axis Reference, Yaw Angle, Average, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAR_YAW_AVG
Description

Solar Axis Reference, Yaw Angle, Average, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sar y avg
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #9
Name
Spacecraft Body Axis, Pitch Angle, Average, GCI
Set
Time series defined by using: EPOCH
ParameterKey
GCI_PITCH_AVG
Description

Spacecraft Body Axis, Pitch Angle, Average, Geocentric Inertial, GCI

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEI
RenderingHints
AxisLabel
GCI p avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #10
Name
Spacecraft Body Axis, Roll Angle, Average, GCI
Set
Time series defined by using: EPOCH
ParameterKey
GCI_ROLL_AVG
Description

Spacecraft Body Axis, Roll Angle, Average, Geocentric Inertial, GCI

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEI
RenderingHints
AxisLabel
GCI r avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #11
Name
Spacecraft Body Axis, Yaw Angle, Average, GCI
Set
Time series defined by using: EPOCH
ParameterKey
GCI_YAW_AVG
Description

Spacecraft Body Axis, Yaw Angle, Average, Geocentric Inertial, GCI

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEI
RenderingHints
AxisLabel
GCI y avg
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #12
Name
Spacecraft Body Axis, Pitch Angle, Average, GSE
Set
Time series defined by using: EPOCH
ParameterKey
GSE_PITCH_AVG
Description

Spacecraft Body Axis, Pitch Angle, Average, Geocentric Solar Ecliptic, GSE

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
GSE p avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #13
Name
Spacecraft Body Axis, Roll Angle, Average, GSE
Set
Time series defined by using: EPOCH
ParameterKey
GSE_ROLL_AVG
Description

Spacecraft Body Axis, Roll Angle, Average, Geocentric Solar Ecliptic, GSE

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
GSE r avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #14
Name
Spacecraft Body Axis, Yaw Angle, Average, GSE
Set
Time series defined by using: EPOCH
ParameterKey
GSE_YAW_AVG
Description

Spacecraft Body Axis, Yaw Angle, Average, Geocentric Solar Ecliptic, GSE

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
AxisLabel
GSE y avg
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #15
Name
Spacecraft Body Axis, Pitch Angle, Average, GSM
Set
Time series defined by using: EPOCH
ParameterKey
GSM_PITCH_AVG
Description

Spacecraft Body Axis, Pitch Angle, Average, Geocentric Solar Magnetospheric, GSM

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
AxisLabel
GSM p avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #16
Name
Spacecraft Body Axis, Roll Angle, Average, GSM
Set
Time series defined by using: EPOCH
ParameterKey
GSM_ROLL_AVG
Description

Spacecraft Body Axis, Roll Angle, Average, Geocentric Solar Magnetospheric, GSM

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
AxisLabel
GSM r avg
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #17
Name
Spacecraft Body Axis, Yaw Angle, Average, GSM
Set
Time series defined by using: EPOCH
ParameterKey
GSM_YAW_AVG
Description

Spacecraft Body Axis, Yaw Angle, Average, Geocentric Solar Magnetospheric, GSM

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
AxisLabel
GSM y avg
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #18
Name
Spacecraft Body Axis, Pitch Angle, Standard Deviation, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_PITCH_STDDEV
Description

Spacecraft Body Axis, Pitch Angle, Standard Deviation, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat p stdv
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
StandardDeviation
SupportQuantity
Positional
Parameter #19
Name
Spacecraft Body Axis, Roll Angle, Standard Deviation, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_ROLL_STDDEV
Description

Spacecraft Body Axis, Roll Angle, Standard Deviation, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat r stdv
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
StandardDeviation
SupportQuantity
Positional
Parameter #20
Name
Spacecraft Body Axis, Yaw Angle, Standard Deviation, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_YAW_STDDEV
Description

Spacecraft Body Axis, Yaw Angle, Standard Deviation, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat r stdv
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
StandardDeviation
SupportQuantity
Positional
Parameter #21
Name
Spacecraft Body Axis, Pitch Angle, Minimum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_PITCH_MIN
Description

Spacecraft Body Axis, Pitch Angle, Minimum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat p min
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Minimum
SupportQuantity
Positional
Parameter #22
Name
Spacecraft Body Axis, Roll Angle, Minimum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_ROLL_MIN
Description

Spacecraft Body Axis, Roll Angle, Minimum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat r min
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Minimum
SupportQuantity
Positional
Parameter #23
Name
Spacecraft Body Axis, Yaw Angle, Minimum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_YAW_MIN
Description

Spacecraft Body Axis, Yaw Angle, Minimum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat y min
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Minimum
SupportQuantity
Positional
Parameter #24
Name
Spacecraft Body Axis, Pitch Angle, Maximum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_PITCH_MAX
Description

Spacecraft Body Axis, Pitch Angle, Maximum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat p max
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Maximum
SupportQuantity
Positional
Parameter #25
Name
Spacecraft Body Axis, Roll Angle, Maximum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_ROLL_MAX
Description

Spacecraft Body Axis, Roll Angle, Maximum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat r max
ValueFormat
F9.5
ScaleMin
-3.14159
ScaleMax
3.14159
ValidMin
-3.14159
ValidMax
3.14159
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Maximum
SupportQuantity
Positional
Parameter #26
Name
Spacecraft Body Axis, Yaw Angle, Maximum, HEC
Set
Time series defined by using: EPOCH
ParameterKey
SAT_YAW_MAX
Description

Spacecraft Body Axis, Yaw Angle, Maximum, Heliospheric Ecliptic, HEC

Cadence
PT10M
Units
rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
HEE
RenderingHints
AxisLabel
Sat y max
ValueFormat
F9.5
ScaleMin
-1.5708
ScaleMax
1.5708
ValidMin
-1.5708
ValidMax
1.5708
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
Qualifier
Maximum
SupportQuantity
Positional