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Pléiades (satellite)

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French Earth observation satellite
Pléiades-1A and Pléiades-1B
Pléiades satellite
Mission typeEarth observation/Reconnaissance
OperatorCNES
COSPAR ID 1A: 2011-076F
1B: 2012-068A
SATCAT no. 1A: 38012
1B: 39019
WebsiteCNES (Pléiades satellites)
Mission duration5 years (planned)
Spacecraft properties
Bus Astrosat-1000
ManufacturerEADS Astrium Satellites
Launch mass970 kg (2,140 lb) (each)
Start of mission
Launch date1A: 02:03, 17 December 2011 (UTC) (2011年12月17日T02:03:00Z)
1B: 02:02, 2 December 2012 (UTC) (2012年12月02日T02:02:00Z)
RocketSoyuz ST-A / Fregat
Launch siteCentre Spatial Guyanais, ELS
Orbital parameters
Reference systemGeocentric orbit
RegimeSun-synchronous orbit
Altitude695 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.

History

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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.

Launches

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Technologies

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Orbit

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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]

  • Orbit: Sun-synchronous, phased, near-circular
  • Mean altitude: 695 km

Equipment

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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.

Agility for Responsive Tasking

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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:

  • Image acquisition anywhere within an 800-km-wide ground strip with 70 cm of resolution
  • Along-track stereo and tri-stereo image acquisition
  • Single-pass collection of mosaics (strip-mapping) with a footprint up to a square degree
  • Maximum theoretical acquisition capacity of 1,000,000 km2 per day and per satellite
  • Optimized daily acquisition capacity (taking into account genuine order book, weather constraints, conflicts...) reaching 300,000 km2 per day and per satellite

Products

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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

[6]

Ground receiving stations

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When satellite operations begin, four ground receiving stations will be deployed for the direct downlink and archiving of imagery data:

  • Two defence centres in France and Spain
  • Two civil stations: one in Toulouse (France) and a polar station in Kiruna (Sweden), which receives most of the data

Regional receiving stations (fixed or mobile) are subsequently installed at the request of users.

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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]

See also

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References

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January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Earth reconnaissance satellites (excluding China, Russia and the United States)
France France
IMINT
SIGINT
Germany Germany
Radar IMINT
India India
IMINT
Radar IMINT
SIGINT
Israel Israel
IMINT
Radar IMINT
Italy Italy
Radar IMINT
Japan Japan
IMINT
Pakistan Pakistan
IMINT
South Korea South Korea
IMINT
Spain Spain
Radar IMINT
Turkey Turkey
IMINT
United Kingdom United Kingdom
IMINT

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