dbo:SpaceMission/missionDuration
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dbo:abstract
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- 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)
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dbo:cosparId
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dbo:launchDate
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dbo:launchVehicle
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dbo:manufacturer
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dbo:missionDuration
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- 473364000.000000 (xsd:double)
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dbo:nextMission
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dbo:operator
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dbo:previousMission
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dbo:satcat
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dbo:type
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dbo:wikiPageExternalLink
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dbo:wikiPageID
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dbo:wikiPageLength
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- 5406 (xsd:nonNegativeInteger)
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dbo:wikiPageRevisionID
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dbo:wikiPageWikiLink
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dbp:apsis
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dbp:cosparId
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dbp:launchContractor
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dbp:launchDate
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- 0001-08-04 (xsd:gMonthDay)
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dbp:launchRocket
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dbp:launchSite
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dbp:manufacturer
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dbp:missionDuration
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dbp:missionType
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dbp:name
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dbp:nextMission
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dbp:operator
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dbp:orbitEpoch
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- 0001-10-29 (xsd:gMonthDay)
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dbp:orbitInclination
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dbp:orbitLongitude
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dbp:orbitPeriod
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dbp:orbitReference
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dbp:orbitRegime
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dbp:power
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dbp:previousMission
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dbp:satcat
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dbp:spacecraftBus
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dbp:transBand
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- 4 (xsd:integer)
- 24 (xsd:integer)
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dbp:transBandwidth
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dbp:transCoverage
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dbp:wikiPageUsesTemplate
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dcterms:subject
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gold:hypernym
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rdf:type
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rdfs:comment
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- 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)
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rdfs:label
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- نايل سات 201 (ar)
- Nilesat 201 (de)
- Nilesat 201 (en)
- Nilesat 201 (pt)
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owl:sameAs
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prov:wasDerivedFrom
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foaf:isPrimaryTopicOf
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foaf:name
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