Pléiades (satellite)

Pléiades-1A and Pléiades-1B
Pléiades satellite
Mission typeEarth observation
OperatorCNES
COSPAR ID1A: 2011-076F
1B: 2012-068A
SATCAT no.1A: 38012
1B: 39019
WebsiteCNES (Pléiades satellites)
Mission duration5 years (planned)
Spacecraft properties
BusAstrosat-1000
ManufacturerEADS Astrium Satellites
Launch mass970 kg (2,140 lb) (each)
Start of mission
Launch date1A: 02:03, 17 December 2011 (UTC) (2011-12-17T02:03Z)
1B: 02:02, 2 December 2012 (UTC) (2012-12-02T02:02Z)
RocketSoyuz ST-A / Fregat
Launch siteCentre Spatial Guyanais, ELS
Orbital parameters
Reference systemGeocentric orbit
RegimeSun-synchronous orbit
Altitude695 km (432 mi)
Inclination98.2°
 

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. 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

The Pléiades system was designed under the French-Italian ORFEO Programme (Optical and Radar Federated Earth Observation) between 2001 and 2003.

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

Technologies

Orbit

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.

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

Equipment

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

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

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

Ground receiving stations

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.

Uplink Stations

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.

See also


This page was last updated at 2024-03-28 16:17 UTC. Update now. View original page.

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