Pléiades satellite
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| Mission type | Earth observation |
|---|---|
| Operator | CNES |
| COSPAR ID | 1A: 2011-076F 1B: 2012-068A |
| SATCAT no. | 1A: 38012 1B: 39019 |
| Website | CNES (Pléiades satellites) |
| Mission duration | 5 years (planned) |
| Spacecraft properties | |
| Bus | Astrosat-1000 |
| Manufacturer | EADS Astrium Satellites |
| Launch mass | 970 kg (2,140 lb) (each) |
| Start of mission | |
| Launch date | 1A: 02:03, 17 December 2011 (UTC) (2011-12-17T02:03Z) 1B: 02:02, 2 December 2012 (UTC) (2012-12-02T02:02Z) |
| Rocket | Soyuz ST-A / Fregat |
| Launch site | Centre Spatial Guyanais, ELS |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Sun-synchronous orbit |
| Altitude | 695 km (432 mi) |
| Inclination | 98.2° |
The Pléiades constellation is composed of two very-high-resolution optical Earth-imaging satellites. Pléiades-1A and Pléiades-1B provide the coverage of Earth's surface with a repeat cycle of 26 days.[1] Designed as a dual civil/military system, Pléiades will meet the space imagery requirements of European defence as well as civil and commercial needs.
The Pléiades system was designed under the French-Italian ORFEO Programme (Optical and Radar Federated Earth Observation) between 2001 and 2003.[2]
The Pléiades programme was launched in October 2003 with CNES (the French space agency) as the overall system prime contractor and EADS Astrium as the prime contractor for the space segment.
Spot Image is the official and exclusive worldwide distributor of Pléiades products and services under a delegated public service agreement.
The two satellites operate in the same phased orbit and are offset at 180° to offer a daily revisit capability over any point on the globe. The Pléiades also share the same orbital plane as the SPOT 6 and 7, forming a larger constellation with 4 satellites, 90° apart from one another.[5]
Equipped with technologies like fibre-optic gyroscopes and control moment gyroscopes, Pléiades-HR 1A, and 1B offer roll, pitch, and yaw (slew) agility, enabling the system to maximize the number of acquisitions above a given area.
This agility coupled with particularly dynamic image acquisition programming make the Pléiades system very responsive to specific user requirements. Individual user requests was answered in record time, thanks to multiple programming plans per day and a state-of-the-art image processing chain. Performance at a glance:
| Resolution | Panchromatic: 50 cm |
| Multispectral: 2 m | |
| Pansharpened: 50 cm | |
| Bundle: 50 cm PAN and 2 m MS | |
| Footprint | 20 km swath |
| Single pass mosaics up to 100 x 100 km |
When satellite operations begin, four ground receiving stations will be deployed for the direct downlink and archiving of imagery data:
Regional receiving stations (fixed or mobile) are subsequently installed at the request of users.
The Pléiades tasking plan are refreshed and uploaded three times per day, allowing for last minute requests and the ability to utilize up-to-the-minute weather forecasts.[7]
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Earth reconnaissance satellites (excluding Russia and the United States)
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