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{{Infobox spaceflight
{{Infobox spaceflight
| name = Pléiades 1A, Pléiades 1B
| name = Pléiades-HR 1A, Pléiades-HR 1B
| names_list = <!--list of previous names if the spacecraft has been renamed.
| names_list = <!--list of previous names if the spacecraft has been renamed.
Include the dates applicable if possible, and separate each name with a linebreak.
Include the dates applicable if possible, and separate each name with a linebreak.
Omit if the spacecraft has only ever been known by one name.
Omit if the spacecraft has only ever been known by one name.
Do not include Harvard, COSPAR/NSSDC or SATCAT/NORAD/NASA designations as alternative names-->
Do not include Harvard, COSPAR/NSSDC or SATCAT/NORAD/NASA designations as alternative names-->


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| operator = [[CNES]]
| operator = [[CNES]]
| Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)-->
| Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)-->
| COSPAR_ID = '''1A''': 2011-076F<br>'''1B''': 2012-068A
| COSPAR_ID = '''1A''': 2011-076F<br/>'''1B''': 2012-068A
| SATCAT = '''1A''': 38012<br>'''1B''': 39019
| SATCAT = '''1A''': 38012<br/>'''1B''': 39019
| website = [http://smsc.cnes.fr/PLEIADES/ At CNES.fr]
| website = [http://smsc.cnes.fr/PLEIADES/ At CNES.fr]
| mission_duration = 5 years (planned)
| mission_duration = 5 years (planned)
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| spacecraft_type = <!--eg. GPS Block II, Kobalt-M, US-K, etc-->
| spacecraft_type = <!--eg. GPS Block II, Kobalt-M, US-K, etc-->
| spacecraft_bus = [[Astrosat-1000]]
| spacecraft_bus = [[Astrosat-1000]]
| manufacturer = [[EADS Astrium]]
| manufacturer = [[EADS Astrium]]
| launch_mass = {{convert|970|kg|abbr=on}} each
| launch_mass = {{convert|970|kg|abbr=on}} each
| BOL_mass = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase-->
| BOL_mass = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase-->
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<!--Launch details-->
<!--Launch details-->
| launch_date = '''1A''': {{start date|2011|12|17|02|03||TZ=Z}}<br>'''1B''': {{start date|2012|12|02|02|02||TZ=Z}}
| launch_date = '''1A''': {{start date|2011|12|17|02|03||TZ=Z}}<br/>'''1B''': {{start date|2012|12|02|02|02||TZ=Z}}
| launch_rocket = [[Soyuz-2 (rocket)#Soyuz 2.1a|Soyuz STA]] with [[Fregat]] upper stage
| launch_rocket = [[Soyuz-2#Soyuz 2.1a|Soyuz STA]] with [[Fregat]] upper stage
| launch_site = [[Guiana Space Centre]]-[[Ensemble de Lancement Soyouz|ELS]]
| launch_site = [[Guiana Space Centre]]-[[Ensemble de Lancement Soyouz|ELS]]
| launch_contractor = <!--organisation(s) that conducted the launch (eg. United Launch Alliance, Arianespace, etc)-->
| launch_contractor = <!--organisation(s) that conducted the launch (eg. United Launch Alliance, Arianespace, etc)-->
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The following template should be used for ONE of the three above fields "end_of_mission", "decay" or "landing" if the spacecraft is no longer operational.
The following template should be used for ONE of the three above fields "end_of_mission", "decay" or "landing" if the spacecraft is no longer operational.
If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered.
If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered.
{{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown)
{{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown)
-->
-->


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| trans_HPBW = <!--half-power beam width-->
| trans_HPBW = <!--half-power beam width-->


<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions.
<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions.
If in doubt, leave it out-->
If in doubt, leave it out-->
| programme =
| programme =
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The '''Pléiades''' [[Satellite constellation|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.<ref>"[http://smsc.cnes.fr/PLEIADES/GP_systeme.htm Pléiades System CNES]".</ref> Designed as a dual civil/military system, Pléiades will meet the space imagery requirements of [[Europe]]an defence as well as civil and commercial needs.
The '''Pléiades''' [[Satellite constellation|constellation]] is composed of two very-high-resolution optical Earth-imaging satellites. '''Pléiades-HR 1A''' and '''Pléiades-HR 1B''' provide the coverage of Earth’s surface with a repeat cycle of 26 days.<ref>"[http://smsc.cnes.fr/PLEIADES/GP_systeme.htm Pléiades System CNES]".</ref> Designed as a dual civil/military system, Pléiades will meet the space imagery requirements of [[Europe]]an defence as well as civil and commercial needs.


== History ==
== History ==
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[[Spot Image]] is the official and exclusive worldwide distributor of Pléiades products and services under a delegated public service agreement.
[[Spot Image]] is the official and exclusive worldwide distributor of Pléiades products and services under a delegated public service agreement.


==Launches==
== Launches ==
*'''Pléiades 1A''' was launched via a Russian [[Soyuz-2 (rocket)#Soyuz 2.1a|Soyuz STA]] rocket out of the [[Guiana Space Centre]], [[Kourou]], [[French Guiana]], on December 17, 2011, 02:03 UTC.
*'''Pléiades-HR 1A''' was launched via a Russian [[Soyuz-2#Soyuz 2.1a|Soyuz STA]] rocket out of the [[Guiana Space Centre]], [[Kourou]], [[French Guiana]], on December 17, 2011, 02:03 UTC.
*'''Pléiades 1B''' was launched via a Russian [[Soyuz-2 (rocket)#Soyuz 2.1a|Soyuz STA]] rocket out of the [[Guiana Space Centre]], [[Kourou]], [[French Guiana]], on December 2, 2012, 02:02 UTC.<ref>{{cite web|url=http://www.reuters.com/article/2012/12/02/us-space-france-russia-idUSBRE8B101L20121202|title=Soyuz rocket blasts off from French Guiana|work=Reuters}}</ref><ref>{{cite web|url=http://www.forum-conquete-spatiale.fr/t14423p45-lancement-soyouz-st-a-vs04-pleiades-1b-2-decembre-2012|title=Lancement Soyouz-ST-A VS04 / Pléiades-1B - 2 décembre 2012 - Page 4|work=www.forum-conquete-spatiale.fr}}</ref>
*'''Pléiades-HR 1B''' was launched via a Russian [[Soyuz-2#Soyuz 2.1a|Soyuz STA]] rocket out of the [[Guiana Space Centre]], [[Kourou]], [[French Guiana]], on December 2, 2012, 02:02 UTC.<ref>{{cite web|url=http://www.reuters.com/article/2012/12/02/us-space-france-russia-idUSBRE8B101L20121202|title=Soyuz rocket blasts off from French Guiana|work=Reuters}}</ref><ref>{{cite web|url=http://www.forum-conquete-spatiale.fr/t14423p45-lancement-soyouz-st-a-vs04-pleiades-1b-2-decembre-2012|title=Lancement Soyouz-ST-A VS04 / Pléiades-1B - 2 décembre 2012 - Page 4|work=www.forum-conquete-spatiale.fr}}</ref>


== Technologies ==
== Technologies ==
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=== Innovation ===
=== Innovation ===
Equipped with innovative latest-generation space technologies like fibre-optic gyros and control moment gyros, Pléiades 1A and 1B will offer exceptional roll, pitch and yaw (slew) agility, enabling the system to maximize the number of acquisitions above a given area.
Equipped with innovative latest-generation space technologies like fibre-optic gyros and control moment gyros, Pléiades-HR 1A and 1B will offer exceptional roll, pitch and yaw (slew) agility, enabling the system to maximize the number of acquisitions above a given area.


=== Agility for Responsive Tasking ===
=== Agility for Responsive Tasking ===
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* Optimized daily acquisition capacity (taking into account genuine order book, weather constraints, conflicts...) reaching 300,000&nbsp;km<sup>2</sup> per day and per satellite.
* Optimized daily acquisition capacity (taking into account genuine order book, weather constraints, conflicts...) reaching 300,000&nbsp;km<sup>2</sup> per day and per satellite.


=== Products===
=== Products ===


{|class="wikitable" width="60%" align="center"
{|class="wikitable" width="60%" align="center"
|-
|-
|align="center" |'''Resolution'''
|align="center" |'''Resolution'''
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|-
|-
|
|
|align="left" |Pansharpened: 50&nbsp;cm ,
|align="left" |Pansharpened: 50&nbsp;cm ,
|-
|-
|
|
|align="left" |Bundle: 50&nbsp;cm PAN & 2 m MS
|align="left" |Bundle: 50&nbsp;cm PAN & 2 m MS
|-
|-
|align="center" |'''Footprint'''
|align="center" |'''Footprint'''
|align="left" |20&nbsp;km swath
|align="left" |20&nbsp;km swath
|-
|-
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Regional receiving stations (fixed or mobile) will subsequently be installed at the request of users.
Regional receiving stations (fixed or mobile) will subsequently be installed at the request of users.


===Uplink Stations ===
=== Uplink Stations ===
The Pléiades tasking plan will be refreshed and uploaded three times per day, allowing for last minute requests and the ability to utilize up-to-the-minute weather forecasts.<ref>"[http://www.spotimage.fr/automne_modules_files/standard/public/SM46_vo_pleiades.pdf Pléiades Responsive Stations]".</ref>
The Pléiades tasking plan will be refreshed and uploaded three times per day, allowing for last minute requests and the ability to utilize up-to-the-minute weather forecasts.<ref>"[http://www.spotimage.fr/automne_modules_files/standard/public/SM46_vo_pleiades.pdf Pléiades Responsive Stations]".</ref>
* The [[Kerguelen Island]] station uploads the morning pass, over Europe, Africa and the Middle East.
* The [[Kerguelen Island]] station uploads the morning pass, over Europe, Africa and the Middle East.
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{{Orbital launches in 2012}}
{{Orbital launches in 2012}}


[[Category:Satellites of France]]
[[Category:Reconnaissance satellites of France]]
[[Category:Earth observation satellites]]
[[Category:Spacecraft launched by Soyuz-2 rockets]]
[[Category:Remote sensing]]
[[Category:Spacecraft launched in 2011]]
[[Category:Spacecraft launched in 2011]]
[[Category:Spacecraft launched in 2012]]
[[Category:Spacecraft launched in 2012]]
[[Category:Reconnaissance satellites of France]]
[[Category:Satellite imagery]]

Revision as of 00:50, 2 January 2017

Pléiades-HR 1A, Pléiades-HR 1B
Mission typeEarth observation
OperatorCNES
COSPAR ID1A: 2011-076F
1B: 2012-068A
SATCAT no.1A: 38012
1B: 39019
WebsiteAt CNES.fr
Mission duration5 years (planned)
Spacecraft properties
BusAstrosat-1000
ManufacturerEADS Astrium
Launch mass970 kg (2,140 lb) each
Start of mission
Launch date1A: 02:03, December 17, 2011 (2011-12-17T02:03)
1B: 02:02, December 2, 2012 (2012-12-02T02:02)
RocketSoyuz STA with Fregat upper stage
Launch siteGuiana Space Centre-ELS
Orbital parameters
Reference systemGeocentric
Regimesun-synchronous
Eccentricity~0
Perigee altitude695 km (432 mi)
Apogee altitude695 km (432 mi)
Inclination98.2


The Pléiades constellation is composed of two very-high-resolution optical Earth-imaging satellites. Pléiades-HR 1A and Pléiades-HR 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 program (Optical & 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

Technologies

Orbit

The two satellites operate in the same phased orbit and will be 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: 694 km.

Innovation

Equipped with innovative latest-generation space technologies like fibre-optic gyros and control moment gyros, Pléiades-HR 1A and 1B will offer exceptional 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 will make the Pléiades system very responsive to specific user requirements. Individual user requests will be 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 & 2 m MS
Footprint 20 km swath
Single pass mosaics up to 100 km 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 will receive most of the data.

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

The Pléiades tasking plan will be 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.

Applications of VHR imagery

The Pléiades system is designed for a range of very-high-resolution (VHR) remote sensing applications. These include:

  • Land planning: detection and identification of small features (e.g. vehicles, roads, bushes)
  • Agriculture: land management and crop yields, location of crop diseases, tree count (palm trees, vineyards...)
  • Defense: imagery-derived intelligence and tactical planning in urban/densely populated areas
  • Homeland Security: mitigation, assistance in crisis events and post-crisis assessment (particularly earthquakes)
  • Hydrology: topography and drainage basin gradient studies
  • Forestry: illicit deforestation and management of forestry yields; REDD data qualification (sampling)
  • Maritime and littoral surveillance: vessel reconnaissance and contamination (oil spill), harbor mapping
  • Civil Engineering/Asset Monitoring: planning of road, rail and oil pipeline corridors
  • 3D: flight simulators, high precision mapping, photovoltaic fields implantation...

See also

References

  1. ^ "Pléiades System CNES".
  2. ^ "Pléiades CNES Mag".
  3. ^ "Soyuz rocket blasts off from French Guiana". Reuters.
  4. ^ "Lancement Soyouz-ST-A VS04 / Pléiades-1B - 2 décembre 2012 - Page 4". www.forum-conquete-spatiale.fr.
  5. ^ "Pleiades eoPortal Directory". eoPortal. Retrieved 2015-06-04.
  6. ^ "Pléiades Products CNES".
  7. ^ "Pléiades Responsive Stations".
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