Pléiades (satellite)
Pléiades satellite | |
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.
History
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
- Pléiades-1A was launched via a Russian Soyuz ST-A launch vehicle of the Centre Spatial Guyanais, Kourou, French Guiana, on 17 December 2011 at 02:03 UTC.
- Pléiades-1B was launched via a Russian Soyuz ST-A launch vehicle of the Centre Spatial Guyanais, Kourou, French Guiana, on 2 December 2012 at 02:02 UTC.[3][4]
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.[5]
- 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 |
[6]
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.[7]
- The Kerguelen Island station uploads the morning pass, over Europe, Africa and the Middle East.
- The Swedish station takes care of midday orbits, over North and South Americas.
- The French station transmits the last tasking plan of the day over Asia and Oceania.
See also
- Geographic information system (GIS)
- Remote sensing
- Pléiades Neo [fr]
References
- ^ "Pléiades System CNES"
- ^ "Pléiades CNES Mag Archived 20 July 2011 at the Wayback Machine"
- ^ "Soyuz rocket blasts off from French Guiana". Reuters. 2 December 2012.
- ^ "Lancement Soyouz-ST-A VS04 / Pléiades-1B". forum-conquete-spatiale.fr.
- ^ "Pleiades eoPortal Directory". eoPortal. Retrieved 4 June 2015.
- ^ "Pléiades Products CNES"
- ^ "Pléiades Responsive Stations"
External links
- Astrium Geo
- ASTRIUM
- CNES
- Gunter's Space Page
- eoportal.org
- v
- t
- e
- Kosmos 2470
- USA-225
- Johannes Kepler ATV
- STS-133 (Leonardo)
- Kosmos 2471
- Glory, Explorer-1 [Prime], KySat-1, Hermes
- USA-226
- USA-227
- Shijian XI-03
- STS-135 (Raffaello, PSSC-2)
- Tianlian I-02
- Globalstar M083, Globalstar M088, Globalstar M091, Globalstar M085, Globalstar M081, Globalstar M089
- GSAT-12
- SES-3, KazSat-2
- USA-232
- Spektr-R
- Compass-IGSO4
- Shijian XI-02
- Juno
- Astra 1N, BSAT-3c/JCSAT-110R
- Paksat-1R
- Hai Yang 2A
- Sich 2, NigeriaSat-2, NigeriaSat-X, RASAT, EduSAT, AprizeSat-5, AprizeSat-6, BPA-2
- Ekspress-AM4
- Shijian XI-04
- Progress M-12M
- GRAIL-A , GRAIL-B
- Zhongxing-1A
- Kosmos 2473
- Arabsat 5C, SES-2
- IGS Optical 4
- Atlantic Bird 7
- TacSat-4
- Tiangong-1
- QuetzSat 1
- Kosmos 2475 , Kosmos 2476 , Kosmos 2477
- Fobos-Grunt , Yinghuo-1
- Yaogan 12 , Tian Xun-1
- Soyuz TMA-22
- Shiyan Weixing 4 , Chuang Xin 1C
- AsiaSat 7
- Mars Science Laboratory (Curiosity)
- Kosmos 2478
- Yaogan 13
- Compass-IGSO5
- Amos-5, Luch 5A
- IGS Radar 3
- Pléiades-HR 1A, SSOT, ELISA 1, ELISA 2, ELISA 3, ELISA 4
- NigComSat-1R
- Soyuz TMA-03M
- Ziyuan-1C
- Meridian 5
- Globalstar M080, Globalstar M082, Globalstar M084, Globalstar M086, Globalstar M090, Globalstar M092
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).