Pléiades (satellite)

{{Short description|French Earth observation satellite}}

{{Use British English|date=June 2020}}

{{Use dmy dates|date=June 2020}}

{{Infobox spaceflight

| name = Pléiades-1A and Pléiades-1B

| names_list =

| image = Pléiades (satellite).jpg

| image_caption = Pléiades satellite

| image_size = 300px

| mission_type = Earth observation/Reconnaissance

| operator = CNES

| COSPAR_ID = 1A: 2011-076F
1B: 2012-068A

| SATCAT = 1A: 38012
1B: 39019

| website = [https://pleiades.cnes.fr/en/PLEIADES/index.htm CNES (Pléiades satellites)]

| mission_duration = 5 years (planned)

| spacecraft =

| spacecraft_type =

| spacecraft_bus = Astrosat-1000

| manufacturer = EADS Astrium Satellites

| launch_mass = {{cvt|970|kg}} (each)

| dimensions =

| power =

| launch_date = 1A: {{start date|df=yes|2011|12|17|02|03|7=Z}}
1B: {{start date|df=yes|2012|12|02|02|02|7=Z}}

| launch_rocket = Soyuz ST-A / Fregat

| launch_site = Centre Spatial Guyanais, ELS

| launch_contractor =

| entered_service =

| disposal_type =

| deactivated =

| destroyed =

| last_contact =

| orbit_reference = Geocentric orbit

| orbit_regime = Sun-synchronous orbit

| orbit_altitude = {{cvt|695|km}}

| orbit_inclination = 98.2°

| orbit_period =

| apsis = gee

| insignia =

| insignia_caption =

| insignia_size = 200px

| programme =

| previous_mission =

| next_mission =

}}

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."[http://smsc.cnes.fr/PLEIADES/GP_systeme.htm Pléiades System CNES]" 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."[http://www.cnes-multimedia.fr/cnes_fr/cnesmag/cnesmag17_FR_cooperation.pdf Pléiades CNES Mag] {{Webarchive|url=https://web.archive.org/web/20110720212252/http://www.cnes-multimedia.fr/cnes_fr/cnesmag/cnesmag17_FR_cooperation.pdf |date=20 July 2011 }}"

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.{{cite news|url=https://www.reuters.com/article/us-space-france-russia-idUSBRE8B101L20121202|title=Soyuz rocket blasts off from French Guiana|work=Reuters|date=2 December 2012}}{{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|publisher=forum-conquete-spatiale.fr}}

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.{{cite web|url=https://directory.eoportal.org/web/eoportal/satellite-missions/p/pleiades

|title=Pleiades eoPortal Directory|publisher=eoPortal|access-date=2015-06-04}}

  • 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 =

class="wikitable" width="60%" align="center"
align="center" | Resolution

|align="left" | Panchromatic: 50 cm

|align="left" | Multispectral: 2 m
|align="left" | Pansharpened: 50 cm
|align="left" | Bundle: 50 cm PAN and 2 m MS
align="center" | Footprint

|align="left" | 20 km swath

|align="left" | Single pass mosaics up to 100 x 100 km
"[http://smsc.cnes.fr/PLEIADES/A_produits.htm Pléiades Products CNES]"

= 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.

See also

{{Portal|Spaceflight}}

References

{{Reflist|30em}}