spase://NASA/NumericalData/ELFIN/B/Ephemeris/PT1S

ResourceName

ELFIN B Ephemeris (State) CubeSat Position, Velocity, Attitude, Spin Rate, and Spin Phase, Level 1 (L1), 1 s Data

ReleaseDate

2021-03-29 17:14:50Z

Description

The Electron Losses and Fields Investigation (ELFIN) Mission is a Space Weather Mission using three Scientific Instruments in a 3U+ CubeSat. The Instruments measure Wave and Particle Data. This Data Product is a Probe State File that contains CubeSat Position, Velocity, Spin Attitude, Spin Rate, and Spin Phase Data.

Acknowledgement

Please acknowledge the Principal Investigator, V. Angelopoulos, NASA, and NSF for providing the Data. Open Data for Scientific Use.

Contacts

	Role	Person
1.	PrincipalInvestigator	spase://SMWG/Person/Vassilis.Angelopoulos
2.	MetadataContact	spase://SMWG/Person/Robert.M.Candey
3.	MetadataContact	spase://SMWG/Person/Lee.Frost.Bargatze

InformationURL

Name

ELFIN Mission Overview Web Page, UCLA

URL

https://elfin.igpp.ucla.edu/about

Description

Electron Losses and Fields Investigation, ELFIN, Mission Overview Web Page, University of California, Los Angeles

InformationURL

Name

ELFIN Attitude Determination and Control Subsystem Web Page, UCLA

URL

https://elfin.igpp.ucla.edu/adcs

Description

ELFIN Attitude Determination and Control Subsystem, ADCS, Web Page, University of California, Los Angeles

PriorIDs

spase://VSPO/NumericalData/ELFIN/B/Ephemeris/PT1S

RepositoryID

spase://SMWG/Repository/NASA/GSFC/SPDF

Availability

Online

AccessRights

Open

AccessURL

Name

FTPS from SPDF (not with most browsers)

URL

ftps://spdf.gsfc.nasa.gov/pub/data/elfin/elfinb/ephemeris

Description

Access to Data in CDF Format via ftp from SPDF

AccessURL

Name

HTTPS from SPDF

URL

https://spdf.gsfc.nasa.gov/pub/data/elfin/elfinb/ephemeris

Description

Access to Data in CDF Format via http from SPDF

AccessURL

Name

CDAWeb

URL

https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=ELB_L1_STATE&index=sp_phys

ProductKey

ELB_L1_STATE

Description

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

Format

CDF

Encoding

None

Acknowledgement

Please acknowledge the Principal Investigator, V. Angelopoulos, NASA, and NSF for providing the Data. Open Data for Scientific Use. Please acknowledge the Data Providers and CDAWeb when using these Data.

RepositoryID

spase://SMWG/Repository/NASA/GSFC/SPDF

Availability

Online

AccessRights

Open

AccessURL

Name

CDAWeb Programmatic Data Access

URL

https://cdaweb.gsfc.nasa.gov/WS/cdasr/1/dataviews/sp_phys/datasets/ELB_L1_STATE/clientLibraryExample/

Style

WebService

ProductKey

ELB_L1_STATE

Description

Access to this data from common programming environments. Note: this AccessInformation element was added by HDPWS.

Format

Binary

Acknowledgement

Please acknowledge the Principal Investigator, V. Angelopoulos, NASA, and NSF for providing the Data. Open Data for Scientific Use. Please acknowledge the Data Providers and CDAWeb when using these Data.

Calibrated

spase://SMWG/Instrument/ELFIN/B/Ephemeris

Ephemeris

InstrumentStatus

TimeSpan

StartDate

2018-09-17 00:00:00.000

RelativeStopDate

P6M

Cadence

PT1S

Earth.Magnetosphere

Earth.Magnetosphere.Polar

Earth.NearSurface

Earth.NearSurface.AuroralRegion

Earth.NearSurface.EquatorialRegion

Earth.NearSurface.Ionosphere

Earth.NearSurface.PolarCap

Name

State Time, UTC

ParameterKey

elb_state_time

Description

State Time, UTC, in Seconds since January 1, 2000

Caveats

The State Time is expressed in Unleaped Seconds

Cadence

PT1S

Units

s

RenderingHints

AxisLabel

ELB State Time

ValueFormat

E12.2

ScaleType

LinearScale

ValidMin

2010-01-01T00:00:00.000000000

ValidMax

2030-01-01T00:00:00.999999999

FillValue

9999-12-31T23:59:59.999999999

Support

SupportQuantity

Temporal

Name

CubeSat Position Vector, Geocentric Equatorial Inertial Cartesian Coordinates

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_pos

Description

CubeSat Position Vector, Geocentric Equatorial Inertial, GEI, Cartesian Coordinates

Cadence

PT1S

Units

km

UnitsConversion

1.0e3>m

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GEI

RenderingHints

DisplayType

TimeSeries

ValueFormat

F12.8

Structure

Size

3

Element

Name

X, GEI

Index

1

Element

Name

Y, GEI

Index

2

Element

Name

Z, GEI

Index

3

ValidMin

-1.0e+06

ValidMax

1.0e+06

FillValue

NaN

Support

Qualifier

Vector

SupportQuantity

Positional

Name

CubeSat Velocity Vector, Geocentric Equatorial Inertial Cartesian Coordinates

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_vel

Description

CubeSat Velocity Vector, Geocentric Equatorial Inertial, GEI, Cartesian Coordinates

Cadence

PT1S

Units

km/s

UnitsConversion

1.0e3>m/s

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GEI

RenderingHints

DisplayType

TimeSeries

ValueFormat

F12.8

Structure

Size

3

Element

Name

VX, GEI

Index

1

Element

Name

VY, GEI

Index

2

Element

Name

VZ, GEI

Index

3

ValidMin

-1000.0

ValidMax

1000.0

FillValue

NaN

Support

Qualifier

Vector

SupportQuantity

Positional

Name

CubeSat Spin Axis Attitude, Right Ascension, Geocentric Equatorial Inertial Spherical Coordinates

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_spinras

Description

CubeSat Spin Axis Attitude, Right Ascension, Geocentric Equatorial Inertial, GEI, Spherical Coordinates

Cadence

PT1S

Units

°

UnitsConversion

0.0174532925>rad

CoordinateSystem

CoordinateRepresentation

Spherical

CoordinateSystemName

GEI

RenderingHints

AxisLabel

SpinRas

ValueFormat

F12.8

ValidMin

0.0

ValidMax

360.0

FillValue

NaN

Support

Qualifier

DirectionAngle.AzimuthAngle

Qualifier

Scalar

SupportQuantity

Positional

Name

CubeSat Spin Axis Attitude, Declination, Geocentric Equatorial Inertial Spherical Coordinates

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_spindec

Description

CubeSat Spin Axis Attitude, Declination, Geocentric Equatorial Inertial, GEI, Spherical Coordinates

Cadence

PT1S

Units

°

UnitsConversion

0.0174532925>rad

CoordinateSystem

CoordinateRepresentation

Spherical

CoordinateSystemName

GEI

RenderingHints

AxisLabel

SpinDec

ValueFormat

F12.8

ValidMin

0.0

ValidMax

180.0

FillValue

NaN

Support

Qualifier

DirectionAngle.ElevationAngle

Qualifier

Scalar

SupportQuantity

Positional

Name

CubeSat Spin Period

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_spinper

Description

CubeSat Spin Period, Regularized and Boxcar Averaged

Cadence

PT1S

Units

s

RenderingHints

AxisLabel

SpinPer

ValueFormat

F12.8

ValidMin

0.0

ValidMax

30.0

FillValue

NaN

Support

Qualifier

Scalar

SupportQuantity

Other

Name

CubeSat Maneuver Status Code

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_man

Description

CubeSat Maneuver Status Code

Cadence

PT1S

RenderingHints

AxisLabel

ManCode

ValueFormat

I8

ScaleType

LinearScale

ValidMin

0

ValidMax

4294967295

FillValue

4294967295

Support

Qualifier

Scalar

SupportQuantity

Other

Name

CubeSat Spin Phase

Set

Time Series defined by using: ELB_STATE_TIME

ParameterKey

elb_spinphase

Description

CubeSat Spin Phase

Cadence

PT1S

Units

°

UnitsConversion

0.0174532925>rad

CoordinateSystem

CoordinateRepresentation

Spherical

CoordinateSystemName

GEI

RenderingHints

AxisLabel

SpinPhase

ValueFormat

F12.8

ValidMin

0.0

ValidMax

360.0

FillValue

NaN

Support

Qualifier

DirectionAngle.AzimuthAngle

Qualifier

Scalar

SupportQuantity

Positional

ELFIN B Ephemeris (State) CubeSat Position, Velocity, Attitude, Spin Rate, and Spin Phase, Level 1 (L1), 1 s Data

Details

NumericalData