Version:2.2.9

NumericalData

ResourceHeader

ResourceName

Interball Tail definitive orbital data

ReleaseDate

2019-08-05 15:03:35Z

Description

Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags.

Acknowledgement

The Interball project, Russian Space Research Institute (IKI) and Dr. Prokhorenko

Contacts

	Role	Person
1.	PrincipalInvestigator	spase://SMWG/Person/Victoria.I.Prokhorenko
2.	MetadataContact	spase://SMWG/Person/Jan.Merka

InformationURL

Name

IKI Satellite Situation Center

URL

http://www.iki.rssi.ru/vprokhor/

Description

This page maintains the Situation Analysis for the IKI International Space Missions and its coordination with the Inter-Agency multimission campaigns.

InformationURL

Name

Interball Tail Probe Situation Analysis

URL

http://www.iki.rssi.ru/vprokhor/tail.htm

PriorIDs

spase://VMO/NumericalData/Interball-Tail/Ephemeris/PT2M

AccessInformation

RepositoryID

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

Availability

Online

AccessRights

Open

AccessURL

Name

FTP access to files at SPDF

URL

ftps://cdaweb.gsfc.nasa.gov/pub/data/interball/tail/orbit/

Description

In CDF via FTP from CDAWeb

AccessURL

Name

HTTP access to files at SPDF

URL

https://spdf.gsfc.nasa.gov/pub/data/interball/tail/orbit/

Description

In CDF via HTTP from CDAWeb

Format

CDF

Encoding

None

AccessInformation

RepositoryID

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

Availability

Online

AccessRights

Open

AccessURL

Name

CDAWeb

URL

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

ProductKey

IT_OR_DEF

Description

Interball Tail definitive orbital data with subset, plot, and list functionalities from CDAWeb.

AccessURL

Name

SSCWeb

URL

https://sscweb.gsfc.nasa.gov/cgi-bin/Locator.cgi

ProductKey

interballtail

Format

Text

Encoding

None

MeasurementType

Ephemeris

TemporalDescription

TimeSpan

StartDate

1995-08-07 00:00:00Z

StopDate

2000-10-16 13:55:00.00Z

Cadence

PT2M

ObservedRegion

Heliosphere.NearEarth

ObservedRegion

Earth.Magnetosheath

ObservedRegion

Earth.Magnetosphere

ObservedRegion

Earth.Magnetosphere.Main

ObservedRegion

Earth.Magnetosphere.Polar

Caveats

The data cadence varies.

Parameter #1

Name

Time

ParameterKey

Epoch

Description

Time (centered) in miliseconds since CDF epoch

Units

ms

UnitsConversion

1e-3>s

ValidMin

01-Jan-1994 00:00:00.000

ValidMax

31-Dec-2020 23:59:59.000

FillValue

-1.0E31

Support

SupportQuantity

Temporal

Parameter #2

Name

I1 position in GSE

ParameterKey

SC_pos_GSE

Description

Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km)

Units

Re

UnitsConversion

6.37e6>m

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GSE

RenderingHints

ValueFormat

F7.3

Structure

Size

3

Element

Name

I1 X (GSE)

Qualifier

Component.I

Index

1

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Element

Name

I1 Y (GSE)

Qualifier

Component.J

Index

2

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Element

Name

I1 Z (GSE)

Qualifier

Component.K

Index

3

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Support

Qualifier

Vector

SupportQuantity

Positional

Parameter #3

Name

I1 S/C position in GSM

ParameterKey

SC_pos_GSM

Description

Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km)

Units

Re

UnitsConversion

6.37e6>m

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GSM

RenderingHints

ValueFormat

F7.3

Structure

Size

3

Element

Name

I1 X (GSM)

Qualifier

Component.I

Index

1

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Element

Name

I1 Y (GSM)

Qualifier

Component.J

Index

2

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Element

Name

I1 Z (GSM)

Qualifier

Component.K

Index

3

ValidMin

-30.0

ValidMax

30.0

FillValue

-1.0E31

Support

Qualifier

Vector

SupportQuantity

Positional

Parameter #4

Name

I1 S/C velocity in GSE

ParameterKey

SC_vel_GSE

Description

Interball-1 spacecraft velocity in km/s in GSE frame

Units

km/s

UnitsConversion

1e3>m/s

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GSE

RenderingHints

ValueFormat

F7.3

Structure

Size

3

Element

Name

I1 Vx (GSE)

Qualifier

Component.I

Index

1

ValidMin

-10.0

ValidMax

10.0

FillValue

-1.0E31

Element

Name

I1 Vy (GSE)

Qualifier

Component.J

Index

2

ValidMin

-10.0

ValidMax

10.0

FillValue

-1.0E31

Element

Name

I1 Vz (GSE)

Qualifier

Component.K

Index

3

ValidMin

-10.0

ValidMax

10.0

FillValue

-1.0E31

Support

Qualifier

Vector

SupportQuantity

Velocity

Parameter #5

Name

SC/SS separation in GSE

ParameterKey

SC/SS_sep_GSE

Description

Satellite-subsatellite separation (Interball-1 - Magion-4) vector in GSE

Units

km

UnitsConversion

1e3>m

CoordinateSystem

CoordinateRepresentation

Cartesian

CoordinateSystemName

GSE

RenderingHints

ValueFormat

F8.1

Structure

Size

3

Element

Name

dx GSE

Qualifier

Component.I

Index

1

ValidMin

-100000.0

ValidMax

100000.0

FillValue

-1.0E31

Element

Name

dy GSE

Qualifier

Component.J

Index

2

ValidMin

-100000.0

ValidMax

100000.0

FillValue

-1.0E31

Element

Name

dz GSE

Qualifier

Component.K

Index

3

ValidMin

-100000.0

ValidMax

100000.0

FillValue

-1.0E31

Support

Qualifier

Vector

SupportQuantity

Positional

Parameter #6

Name

Flag_O

ParameterKey

SF_SC_orbit

Description

Status Flag, Orbit : 0-good data, 1-bad data, 2-missing data

ValidMin

0

ValidMax

5

FillValue

128

Support

SupportQuantity

Other

Parameter #7

Name

Flag_S

ParameterKey

SF_SC_sep

Description

Status Flag, Separation: 0-good data, 1-bad data, 2-missing data

ValidMin

0

ValidMax

5

FillValue

128

Support

SupportQuantity

Other

Parameter #8

Name

Gap Flag

ParameterKey

Gap_Flag

Description

Post Gap Flag: 0 no gap before this point, 1-5 gap reason

ValidMin

0

ValidMax

5

FillValue

-2147483648

Support

SupportQuantity

Other