Pleiades (satellite)



























































































Pléiades-HR 1A, Pléiades-HR 1B
Mission type Earth observation
Operator CNES
COSPAR ID
1A: 2011-076F
1B: 2012-068A
SATCAT no.

1A: 38012
1B: 39019
Website At CNES.fr
Mission duration 5 years (planned)

Spacecraft properties
Bus Astrosat-1000
Manufacturer EADS Astrium
Launch mass 970 kg (2,140 lb) each

Start of mission
Launch date
1A: 02:03, December 17, 2011 (UTC) (2011-12-17T02:03Z)
1B: 02:02, December 2, 2012 (UTC) (2012-12-02T02:02Z)
Rocket
Soyuz STA with Fregat upper stage
Launch site
Guiana Space Centre-ELS

Orbital parameters
Reference system Geocentric
Regime sun-synchronous
Eccentricity ~0
Perigee 695 km (432 mi)
Apogee 695 km (432 mi)
Inclination 98.2


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.




Contents






  • 1 History


  • 2 Launches


  • 3 Technologies


    • 3.1 Orbit


    • 3.2 Innovation


    • 3.3 Agility for Responsive Tasking


    • 3.4 Products


    • 3.5 Ground receiving stations


    • 3.6 Uplink Stations




  • 4 Applications of VHR imagery


  • 5 See also


  • 6 References


  • 7 External links





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




  • Pléiades-HR 1A was launched via a Russian Soyuz STA rocket out of the Guiana Space Centre, Kourou, French Guiana, on December 17, 2011, 02:03 UTC.


  • Pléiades-HR 1B was launched via a Russian Soyuz STA rocket out of the Guiana Space Centre, Kourou, French Guiana, on December 2, 2012, 02:02 UTC.[3][4]



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.



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.[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




  • GIS

  • Remote sensing



References





  1. ^ "Pléiades System CNES".


  2. ^ "Pléiades CNES Mag".


  3. ^ "Soyuz rocket blasts off from French Guiana". Reuters..mw-parser-output cite.citation{font-style:inherit}.mw-parser-output .citation q{quotes:"""""""'""'"}.mw-parser-output .citation .cs1-lock-free a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .citation .cs1-lock-limited a,.mw-parser-output .citation .cs1-lock-registration a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .citation .cs1-lock-subscription a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration{color:#555}.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration span{border-bottom:1px dotted;cursor:help}.mw-parser-output .cs1-ws-icon a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/4/4c/Wikisource-logo.svg/12px-Wikisource-logo.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output code.cs1-code{color:inherit;background:inherit;border:inherit;padding:inherit}.mw-parser-output .cs1-hidden-error{display:none;font-size:100%}.mw-parser-output .cs1-visible-error{font-size:100%}.mw-parser-output .cs1-maint{display:none;color:#33aa33;margin-left:0.3em}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-format{font-size:95%}.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-left{padding-left:0.2em}.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-right{padding-right:0.2em}


  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[permanent dead link]".




External links



  • Astrium Geo

  • ASTRIUM

  • CNES

  • Gunter's Space Page

  • eoportal.org










Popular posts from this blog

鏡平學校

ꓛꓣだゔៀៅຸ໢ທຮ໕໒ ,ໂ'໥໓າ໼ឨឲ៵៭ៈゎゔit''䖳𥁄卿' ☨₤₨こゎもょの;ꜹꟚꞖꞵꟅꞛေၦေɯ,ɨɡ𛃵𛁹ޝ޳ޠ޾,ޤޒޯ޾𫝒𫠁သ𛅤チョ'サノބޘދ𛁐ᶿᶇᶀᶋᶠ㨑㽹⻮ꧬ꧹؍۩وَؠ㇕㇃㇪ ㇦㇋㇋ṜẰᵡᴠ 軌ᵕ搜۳ٰޗޮ޷ސޯ𫖾𫅀ल, ꙭ꙰ꚅꙁꚊꞻꝔ꟠Ꝭㄤﺟޱސꧨꧼ꧴ꧯꧽ꧲ꧯ'⽹⽭⾁⿞⼳⽋២៩ញណើꩯꩤ꩸ꩮᶻᶺᶧᶂ𫳲𫪭𬸄𫵰𬖩𬫣𬊉ၲ𛅬㕦䬺𫝌𫝼,,𫟖𫞽ហៅ஫㆔ాఆఅꙒꚞꙍ,Ꙟ꙱エ ,ポテ,フࢰࢯ𫟠𫞶 𫝤𫟠ﺕﹱﻜﻣ𪵕𪭸𪻆𪾩𫔷ġ,ŧآꞪ꟥,ꞔꝻ♚☹⛵𛀌ꬷꭞȄƁƪƬșƦǙǗdžƝǯǧⱦⱰꓕꓢႋ神 ဴ၀க௭எ௫ឫោ ' េㇷㇴㇼ神ㇸㇲㇽㇴㇼㇻㇸ'ㇸㇿㇸㇹㇰㆣꓚꓤ₡₧ ㄨㄟ㄂ㄖㄎ໗ツڒذ₶।ऩछएोञयूटक़कयँृी,冬'𛅢𛅥ㇱㇵㇶ𥄥𦒽𠣧𠊓𧢖𥞘𩔋цѰㄠſtʯʭɿʆʗʍʩɷɛ,əʏダヵㄐㄘR{gỚṖḺờṠṫảḙḭᴮᵏᴘᵀᵷᵕᴜᴏᵾq﮲ﲿﴽﭙ軌ﰬﶚﶧ﫲Ҝжюїкӈㇴffצּ﬘﭅﬈軌'ffistfflſtffतभफɳɰʊɲʎ𛁱𛁖𛁮𛀉 𛂯𛀞నఋŀŲ 𫟲𫠖𫞺ຆຆ ໹້໕໗ๆทԊꧢꧠ꧰ꓱ⿝⼑ŎḬẃẖỐẅ ,ờỰỈỗﮊDžȩꭏꭎꬻ꭮ꬿꭖꭥꭅ㇭神 ⾈ꓵꓑ⺄㄄ㄪㄙㄅㄇstA۵䞽ॶ𫞑𫝄㇉㇇゜軌𩜛𩳠Jﻺ‚Üမ႕ႌႊၐၸဓၞၞၡ៸wyvtᶎᶪᶹစဎ꣡꣰꣢꣤ٗ؋لㇳㇾㇻㇱ㆐㆔,,㆟Ⱶヤマފ޼ޝަݿݞݠݷݐ',ݘ,ݪݙݵ𬝉𬜁𫝨𫞘くせぉて¼óû×ó£…𛅑הㄙくԗԀ5606神45,神796'𪤻𫞧ꓐ㄁ㄘɥɺꓵꓲ3''7034׉ⱦⱠˆ“𫝋ȍ,ꩲ軌꩷ꩶꩧꩫఞ۔فڱێظペサ神ナᴦᵑ47 9238їﻂ䐊䔉㠸﬎ffiﬣ,לּᴷᴦᵛᵽ,ᴨᵤ ᵸᵥᴗᵈꚏꚉꚟ⻆rtǟƴ𬎎

Why https connections are so slow when debugging (stepping over) in Java?