cosmos.wikisort.org - SpacecraftCerise (French for "cherry") was a French military reconnaissance satellite. Its main purpose was to intercept HF radio signals for French intelligence services.[1] With a mass of 50 kg, it was launched by an Ariane rocket from Kourou in French Guiana at 17:23 UT, 7 July 1995.[1] Cerise's initial orbital parameters were period 98.1 min, apogee 675 km, perigee 666 km, and inclination 98.0 deg.[1]
Cerise Illustration of debris colliding with Cerise |
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Mission type | Military reconnaissance |
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COSPAR ID | 1995-033B  |
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SATCAT no. | 23606 |
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Bus | SSTL-70 |
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Manufacturer | Alcatel Space · Surrey Satellite Technology |
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Launch mass | 50 kg (110 lb) |
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Dry mass | 50kg |
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Dimensions | 0.6 × 0.3 × 0.3 m (1.97 × 0.98 × 0.98 ft) |
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Launch date | 7 July 1995, 16:23:34 (1995-07-07UTC16:23:34) UTC |
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Rocket | Ariane 4 V-75 |
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Launch site | Guiana Space Centre ELA-2 |
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Contractor | Arianespace |
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Reference system | Geocentric |
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Regime | Sun-synchronous |
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Eccentricity | 0.0005756 |
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Perigee altitude | 581 km (361 mi) |
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Apogee altitude | 589 km (366 mi) |
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Inclination | 98.2413° |
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Mean motion | 14.94 rev/day |
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Epoch | 27 December 2016 12:15:03 UTC |
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On 24 July 1996 it was hit by a catalogued space debris object from an Ariane rocket, making it the first verified case of an accidental collision between two artificial objects in space.[2][3]
The collision (with relative velocity of 14.8 km/s) tore off a 2.8-2.9 metre (9.2-9.5 foot) portion of Cerise's gravity-gradient stabilization boom, which left the satellite severely damaged and tumbling with a limited attitude control system. Novel magnetic control algorithms were used to re-stabilise the otherwise undamaged microsatellite to regain almost full operational mission capability.[4][5]
See also
Spaceflight portal
References
External links
Earth reconnaissance satellites (excluding Russia and the United States) |
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China  | IMINT |
- JSSW
- FSW-0
- FSW-1
- FSW-2
- FSW-3
- JianBing
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SIGINT | |
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France  | |
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Germany  | |
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India  | |
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Israel  | |
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Italy  | |
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Japan  | IMINT |
- IGS 1A/B
- IGS 2A/B
- IGS 3A
- IGS 4A/B
- IGS 5A
- IGS 6A
- IGS 7A
- IGS 8A/B
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South Korea  | |
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Spain  | |
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Turkey  | |
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United Kingdom  | |
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← 1994 · Orbital launches in 1995 · 1996 → |
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Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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