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Interball Tail definitive orbital data

ResourceID
spase://NASA/NumericalData/Interball-1/Ephemeris/PT2M

Description

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

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Details

Version:2.3.2

NumericalData

ResourceID
spase://NASA/NumericalData/Interball-1/Ephemeris/PT2M
ResourceHeader
ResourceName
Interball Tail definitive orbital data
ReleaseDate
2021-04-27 15:38:11Z
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
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Victoria.I.Prokhorenko
2.MetadataContactspase://SMWG/Person/Jan.Merka
InformationURL
Name
IKI Satellite Situation Center
URL
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
PriorIDs
spase://VMO/NumericalData/Interball-Tail/Ephemeris/PT2M
spase://VSPO/NumericalData/Interball-1/Ephemeris/PT2M
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTP access to files at SPDF
URL
Description

In CDF via FTP from CDAWeb

AccessURL
Name
HTTPS from SPDF
URL
Description

In CDF via HTTP from CDAWeb

Format
CDF
Encoding
None
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb
URL
ProductKey
IT_OR_DEF
Description

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

AccessURL
Name
SSCWeb
URL
ProductKey
interballtail
Format
Text
Encoding
None
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
IT_OR_DEF
Description

Web Service to this product using the HAPI interface.

Format
CSV
InstrumentIDs
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