[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

About: Nilesat 201

An Entity of Type: Communications satellite, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

Nilesat 201, is an Egyptian communications satellite, which was launched on 4 August 2010. Nilesat 201 will enable the Egyptian satellite operator Nilesat to deliver digital Direct to Home (DTH) TV and radio broadcasting and high-speed data transmission services to North Africa and the Middle East starting in September 2010. It was built by Thales Alenia Space in the Cannes Mandelieu Space Center, and is based on the Spacebus 4000B2 satellite bus. It will be operated in geosynchronous orbit, at a longitude of 7° West. The spacecraft has a design life of 15 years and a mass at launch of 3.2 tonnes. It is powered by solar arrays which will generate 5.9 kilowatts of electricity at the end of the spacecraft's design life. It will carry 40 transponders, of which 24 will be Ku band for broadcast

Property Value
dbo:SpaceMission/missionDuration
  • 5478.75
dbo:abstract
  • هو قمر صناعي مصري وأحد أقمار الجيل الثاني لأقمار النايل سات، أُطلق في الرابع من أغسطس من العام 2010. واستمرت عملية الإقلاع حوالي 27 دقيقة. (ar)
  • Nilesat 201 ist ein kommerzieller Kommunikationssatellit der ägyptischen Firma Nilesat. Nilesat beauftragte Thales Alenia Space im Mai 2008 mit dem Bau des Satelliten, der am 4. August 2010 um 22:59 Uhr MEZ mit einer Trägerrakete vom Typ Ariane 5 ECA vom Raketenstartplatz Kourou in Französisch-Guayana (zusammen mit RASCOM-QAF 1R) in eine geostationäre Transferbahn gebracht wurde. Nilesat 201 sollte weitere Direct-to-Home- Fernseh- und Rundfunkprogramme zur Verfügung stellen (insgesamt mehr als 450 TV-Programme) sowie die High-Speed-Datenübertragung für das Empfangsgebiet in Nordafrika und dem Nahen Osten erweitern. Er sollte damit die bisherigen Satelliten Nilesat 101, 102 und 103 ergänzen. Der Satellit basiert auf dem Satellitenbus B2 von EADS Astrium und verfügt über 24 Ku-Band- und vier Ka-Band-Transponder. Sein Startgewicht beträgt etwa 3200 kg. Der Satellit wird auf der Position 7° West stationiert und hat eine erwartete Lebensdauer von etwa 15 Jahren. (de)
  • Nilesat 201, is an Egyptian communications satellite, which was launched on 4 August 2010. Nilesat 201 will enable the Egyptian satellite operator Nilesat to deliver digital Direct to Home (DTH) TV and radio broadcasting and high-speed data transmission services to North Africa and the Middle East starting in September 2010. It was built by Thales Alenia Space in the Cannes Mandelieu Space Center, and is based on the Spacebus 4000B2 satellite bus. It will be operated in geosynchronous orbit, at a longitude of 7° West. The spacecraft has a design life of 15 years and a mass at launch of 3.2 tonnes. It is powered by solar arrays which will generate 5.9 kilowatts of electricity at the end of the spacecraft's design life. It will carry 40 transponders, of which 24 will be Ku band for broadcasting, and 4 will be Ka band. Nilesat 201 was launched by an Ariane 5ECA rocket at 20:59 UTC on 4 August 2010. (en)
  • O Nilesat 201 é um satélite de comunicação geoestacionário egípcio construído pela Thales Alenia Space. Ele está localizado na posição orbital de 7 graus de longitude oeste e é operado pela Nilesat. O satélite foi baseado na plataforma Spacebus-4000B2 e sua vida útil estimada é de 15 anos. (pt)
dbo:cosparId
  • 2010-037A
dbo:launchDate
  • 2010-08-04 (xsd:date)
dbo:launchVehicle
dbo:manufacturer
dbo:missionDuration
  • 473364000.000000 (xsd:double)
dbo:nextMission
dbo:operator
dbo:previousMission
dbo:satcat
  • 36830
dbo:type
dbo:wikiPageExternalLink
dbo:wikiPageID
  • 17806331 (xsd:integer)
dbo:wikiPageLength
  • 5406 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1105627174 (xsd:integer)
dbo:wikiPageWikiLink
dbp:apsis
  • gee (en)
dbp:cosparId
  • 2010 (xsd:integer)
dbp:launchContractor
dbp:launchDate
  • 0001-08-04 (xsd:gMonthDay)
dbp:launchRocket
  • Ariane 5ECA V196 (en)
dbp:launchSite
dbp:manufacturer
dbp:missionDuration
  • 4.73364E8
dbp:missionType
dbp:name
  • Nilesat 201 (en)
dbp:nextMission
dbp:operator
dbp:orbitEpoch
  • 0001-10-29 (xsd:gMonthDay)
dbp:orbitInclination
  • 0.040000 (xsd:double)
dbp:orbitLongitude
  • 7 (xsd:integer)
dbp:orbitPeriod
  • 86148.0
dbp:orbitReference
dbp:orbitRegime
dbp:power
  • 5700 (xsd:integer)
dbp:previousMission
dbp:satcat
  • 36830 (xsd:integer)
dbp:spacecraftBus
dbp:transBand
  • 4 (xsd:integer)
  • 24 (xsd:integer)
dbp:transBandwidth
  • 33 (xsd:integer)
dbp:transCoverage
dbp:wikiPageUsesTemplate
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • هو قمر صناعي مصري وأحد أقمار الجيل الثاني لأقمار النايل سات، أُطلق في الرابع من أغسطس من العام 2010. واستمرت عملية الإقلاع حوالي 27 دقيقة. (ar)
  • O Nilesat 201 é um satélite de comunicação geoestacionário egípcio construído pela Thales Alenia Space. Ele está localizado na posição orbital de 7 graus de longitude oeste e é operado pela Nilesat. O satélite foi baseado na plataforma Spacebus-4000B2 e sua vida útil estimada é de 15 anos. (pt)
  • Nilesat 201 ist ein kommerzieller Kommunikationssatellit der ägyptischen Firma Nilesat. Nilesat beauftragte Thales Alenia Space im Mai 2008 mit dem Bau des Satelliten, der am 4. August 2010 um 22:59 Uhr MEZ mit einer Trägerrakete vom Typ Ariane 5 ECA vom Raketenstartplatz Kourou in Französisch-Guayana (zusammen mit RASCOM-QAF 1R) in eine geostationäre Transferbahn gebracht wurde. (de)
  • Nilesat 201, is an Egyptian communications satellite, which was launched on 4 August 2010. Nilesat 201 will enable the Egyptian satellite operator Nilesat to deliver digital Direct to Home (DTH) TV and radio broadcasting and high-speed data transmission services to North Africa and the Middle East starting in September 2010. It was built by Thales Alenia Space in the Cannes Mandelieu Space Center, and is based on the Spacebus 4000B2 satellite bus. It will be operated in geosynchronous orbit, at a longitude of 7° West. The spacecraft has a design life of 15 years and a mass at launch of 3.2 tonnes. It is powered by solar arrays which will generate 5.9 kilowatts of electricity at the end of the spacecraft's design life. It will carry 40 transponders, of which 24 will be Ku band for broadcast (en)
rdfs:label
  • نايل سات 201 (ar)
  • Nilesat 201 (de)
  • Nilesat 201 (en)
  • Nilesat 201 (pt)
owl:sameAs
prov:wasDerivedFrom
foaf:isPrimaryTopicOf
foaf:name
  • Nilesat 201 (en)
is dbo:broadcastArea of
is dbo:wikiPageRedirects of
is dbo:wikiPageWikiLink of
is dbp:area of
is foaf:primaryTopic of
Powered by OpenLink Virtuoso    This material is Open Knowledge     W3C Semantic Web Technology     This material is Open Knowledge    Valid XHTML + RDFa
This content was extracted from Wikipedia and is licensed under the Creative Commons Attribution-ShareAlike 3.0 Unported License