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Cluster II was a space mission of the European Space Agency, with NASA participation, to study the Earth's magnetosphere over the course of nearly two solar cycles. The mission was composed of four identical spacecraft flying in a tetrahedral formation. As a replacement for the original Cluster spacecraft which were lost in a launch failure in 1996, the…
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cluster mission space esa solar ii science magnetosphere wind 10 plasma spacecraft satellites scientific years magnetopause magnetic operations double star
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Cluster II (spacecraft) | Apogee altitude | FM6: 116,740 km (72,540 mi) FM7: 116,654 km (72,485 mi) FM5: 116,786 km (72,567 mi) FM8: 119,952 km (74,535 mi) | 1.00 | infobox |
| Cluster II (spacecraft) | Contractor | Starsem | 1.00 | infobox |
| Cluster II (spacecraft) | COSPAR ID | FM6 (SALSA): 2000-041B FM7 (SAMBA): 2000-041A FM5 (RUMBA): 2000-045A FM8 (TANGO): 2000-045B | 1.00 | infobox |
| Cluster II (spacecraft) | Decay date | SALSA: 8 September 2024 RUMBA:22 October 2025 | 1.00 | infobox |
| Cluster II (spacecraft) | Dimensions | 2.9 m × 1.3 m (9.5 ft × 4.3 ft) | 1.00 | infobox |
| Cluster II (spacecraft) | Dry mass | 550 kg (1,210 lb) | 1.00 | infobox |
| Cluster II (spacecraft) | Epoch | 13 March 2014, 11:15:07 UTC | 1.00 | infobox |
| Cluster II (spacecraft) | Inclination | FM6: 135 degrees FM7: 135 degrees FM5: 138 degrees FM8: 134 degrees | 1.00 | infobox |
| Cluster II (spacecraft) | Last contact | 22 August 2024 | 1.00 | infobox |
| Cluster II (spacecraft) | Launch date | FM6: 16 July 2000, 12:39 UTC (2000-07-16UTC12:39Z) FM7: 16 July 2000, 12:39 UTC (2000-07-16UTC12:39Z) FM5: 09 August 2000, 11:13 UTC (2000-08-09UTC11:13Z) FM8: 09 August 2000, 1… | 1.00 | infobox |
| Cluster II (spacecraft) | Launch mass | 1,200 kg (2,600 lb) | 1.00 | infobox |
| Cluster II (spacecraft) | Launch site | Baikonur 31/6 | 1.00 | infobox |
| Cluster II (spacecraft) | Manufacturer | Airbus (ex. Dornier) | 1.00 | infobox |
| Cluster II (spacecraft) | Mission duration | Planned: 5 years Final: 24 years, 1 month and 6 days | 1.00 | infobox |
| Cluster II (spacecraft) | Mission type | Magnetospheric research | 1.00 | infobox |
| Cluster II (spacecraft) | Operator | ESA with NASA collaboration | 1.00 | infobox |
| Cluster II (spacecraft) | Payload mass | 71 kg (157 lb) | 1.00 | infobox |
| Cluster II (spacecraft) | Perigee altitude | FM6: 16,118 km (10,015 mi) FM7: 16,157 km (10,039 mi) FM5: 16,022 km (9,956 mi) FM8: 12,902 km (8,017 mi) | 1.00 | infobox |
| Cluster II (spacecraft) | Period | FM6: 3259 minutes FM7: 3257 minutes FM5: 3257 minutes FM8: 3258 minutes | 1.00 | infobox |
| Cluster II (spacecraft) | Power | 224 watts | 1.00 | infobox |
| Cluster II (spacecraft) | Reference system | Geocentric | 1.00 | infobox |
| Cluster II (spacecraft) | Regime | Elliptical Orbit | 1.00 | infobox |
| Cluster II (spacecraft) | Rocket | Soyuz-U/Fregat | 1.00 | infobox |
| Cluster II (spacecraft) | SATCAT no. | FM6 (SALSA): 26411 FM7 (SAMBA): 26410 FM5 (RUMBA): 26463 FM8 (TANGO): 26464 | 1.00 | infobox |
| Cluster II (spacecraft) | Website | http://sci.esa.int/cluster | 1.00 | infobox |
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