intt-orb-all.xml
7.14 KB
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
<?xml version="1.0" encoding="UTF-8"?>
<Spase xmlns="http://www.spase-group.org/data/schema" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.spase-group.org/data/schema http://cdpp.irap.omp.eu/AMDA-NG/public/schemas/spase-amda-1_2_0.xsd">
<Version>2.2.6</Version>
<NumericalData>
<ResourceID>spase://CDPP/NumericalData/AMDA/Interball-Tail/Ephemeris/intt-orb-all</ResourceID>
<ResourceHeader>
<ResourceName>orbit</ResourceName>
<ReleaseDate>2015-10-16T18:00:00.000</ReleaseDate>
<Description>Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags.</Description>
<Acknowledgement>The Interball project, Russian Space Research Institute (IKI) and Dr. Prokhorenko</Acknowledgement>
<Contact>
<PersonID>spase://SMWG/Person/Victoria.I.Prokhorenko</PersonID>
<Role>PrincipalInvestigator</Role>
</Contact>
<Contact>
<PersonID>spase://SMWG/Person/Elena.Budnik</PersonID>
<Role>TechnicalContact</Role>
</Contact>
<InformationURL>
<Name>IKI Satellite Situation Center</Name>
<URL>http://www.iki.rssi.ru/vprokhor</URL>
<Description>This page maintains the Situation Analysis for the IKI International Space Missions and its coordination with the Inter-Agency multimission campaigns.</Description>
</InformationURL>
<InformationURL>
<Name>Interball Tail Probe Situation Analysis</Name>
<URL>http://www.iki.rssi.ru/vprokhor/tail.htm</URL>
</InformationURL>
</ResourceHeader>
<AccessInformation>
<RepositoryID>spase://SMWG/Repository/CDPP/AMDA</RepositoryID>
<Availability>Online</Availability>
<AccessRights>Open</AccessRights>
<AccessURL>
<Name>AMDA at CDPP</Name>
<URL>http://amda.cdpp.eu</URL>
</AccessURL>
<Format>NetCDF</Format>
<Encoding>None</Encoding>
</AccessInformation>
<ProviderName>CDAWeb</ProviderName>
<InstrumentID>spase://CDPP/Instrument/AMDA/Interball-1/Ephemeris</InstrumentID>
<MeasurementType>Ephemeris</MeasurementType>
<TemporalDescription>
<TimeSpan>
<StartDate>1995-08-04T00:01:00Z</StartDate>
<StopDate>2000-10-16T13:55:00Z</StopDate>
</TimeSpan>
<Cadence>PT2M</Cadence>
</TemporalDescription>
<ObservedRegion>Earth.Magnetosphere</ObservedRegion>
<ObservedRegion>Earth.Magnetosheath</ObservedRegion>
<ObservedRegion>Earth.Magnetosphere.Main</ObservedRegion>
<ObservedRegion>Heliosphere.NearEarth</ObservedRegion>
<Caveats>The data cadence varies.</Caveats>
<Parameter>
<Name>xyz_gse</Name>
<ParameterKey>it_xyz</ParameterKey>
<Description>Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km)</Description>
<Ucd>pos.earth;instr.obsty</Ucd>
<Units>Re</Units>
<UnitsConversion>6.37e6>m</UnitsConversion>
<CoordinateSystem>
<CoordinateRepresentation>Cartesian</CoordinateRepresentation>
<CoordinateSystemName>GSE</CoordinateSystemName>
</CoordinateSystem>
<RenderingHints>
<DisplayType>TimeSeries</DisplayType>
<ValueFormat>F7.3</ValueFormat>
</RenderingHints>
<Structure>
<Size>3</Size>
<Element>
<Name>x</Name>
<Qualifier>Component.I</Qualifier>
<Index>1</Index>
<ParameterKey>it_xyz(0)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>y</Name>
<Qualifier>Component.J</Qualifier>
<Index>2</Index>
<ParameterKey>it_xyz(1)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>z</Name>
<Qualifier>Component.K</Qualifier>
<Index>3</Index>
<ParameterKey>it_xyz(2)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
</Structure>
<Support>
<Qualifier>Vector</Qualifier>
<SupportQuantity>Positional</SupportQuantity>
</Support>
</Parameter>
<Parameter>
<Name>xyz_gsm</Name>
<ParameterKey>it_xyz_gsm</ParameterKey>
<Description>Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km)</Description>
<Ucd>pos.earth;instr.obsty</Ucd>
<Units>Re</Units>
<UnitsConversion>6.37e6>m</UnitsConversion>
<CoordinateSystem>
<CoordinateRepresentation>Cartesian</CoordinateRepresentation>
<CoordinateSystemName>GSM</CoordinateSystemName>
</CoordinateSystem>
<RenderingHints>
<DisplayType>TimeSeries</DisplayType>
<ValueFormat>F7.3</ValueFormat>
</RenderingHints>
<Structure>
<Size>3</Size>
<Element>
<Name>x</Name>
<Qualifier>Component.I</Qualifier>
<Index>1</Index>
<ParameterKey>it_xyz_gsm(0)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>y</Name>
<Qualifier>Component.J</Qualifier>
<Index>2</Index>
<ParameterKey>it_xyz_gsm(1)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
<Element>
<Name>z</Name>
<Qualifier>Component.K</Qualifier>
<Index>3</Index>
<ParameterKey>it_xyz_gsm(2)</ParameterKey>
<ValidMin>-30.0</ValidMin>
<ValidMax>30.0</ValidMax>
<FillValue>-1.0E31</FillValue>
</Element>
</Structure>
<Support>
<Qualifier>Vector</Qualifier>
<SupportQuantity>Positional</SupportQuantity>
</Support>
</Parameter>
</NumericalData>
</Spase>