intelsat iii f‑3

Intelsat 603 or IS-603, previously named Intelsat VI F-3, is a communications satellite operated by Intelsat. ; Polityka prywatności; O Wikipedii; Korzystasz z Wikipedii tylko na własną odpowiedzialność Launched towards geostationary orbit in 1969 it failed to achieve orbit. O Intelsat III F-3 era um satélite de comunicação geoestacionário construído pela TRW, ele era de propriedade da Intelsat, empresa atualmente sediada em Luxemburgo. It had a design life of five years and carried an SVM-2 apogee motor for propulsion.. As of February 3, 2014 it remains in orbit, with a perigee of 39,935 kilometers (24,814 mi), an apogee of 41,521 kilometers (25,800 mi), inclination of 18.63 degrees and an orbital period of 28.25 hours. Intelsat III F-3 was a geostationary communications satellite operated by Intelsat. Satelit Intelsat di orbit géostasionér ampir ngawengku sacara global. Launched in 1994, the satellite was operated by PanAmSat until it merged with Intelsat in 2006. Intelsat 602, also known as IS-602 and previously named Intelsat VI F-2, is a communications satellite operated by Intelsat. The third of four Intelsat II satellites to be launched, Intelsat II F-3 was built by Hughes Aircraft around the HS-303A satellite bus. Intelsat III F-2 was a communications satellite operated by Intelsat. Intelsat II F-4 was a communications satellite operated by Intelsat. The Intelsat VI series was constructed by Hughes Aircraft, based on the HS-389 satellite bus. The third of eight Intelsat III satellites to be launched, Intelsat III F-3 was built by TRW. Launched in 1989, it was the first of five Intelsat VI satellites to be launched. Launch Complex: Cape Canaveral LC17A. Topic. [4]. Intelsat III F-3 Intelsat III F-4 Goonhilly and Raisting Intelsat II F-1 bija Intelsat sakaru pavadonis, kas 1966. gada oktobrī kļūmes dēļ ievadīts nepareizā orbītā. [1] Shortly after launch, Intelsat III F-3 fired its apogee motor to achieve geostationary orbit. Intelsat II F-3, also known as Canary Bird was a communications satellite operated by Intelsat. 1969 February 6 - .00:39 GMT - . [4], "INTELSAT 3-F3 Satellite details 1969-011A NORAD 03674", "Chronology of Intelsat Development and Operations, 1969-1978", https://en.wikipedia.org/w/index.php?title=Intelsat_III_F-3&oldid=1000952235, All Wikipedia articles written in American English, Creative Commons Attribution-ShareAlike License, This page was last edited on 17 January 2021, at 14:46. Línguas. Launched in 1969 it was intended for operations over the Pacific Ocean; however, it spent most of its service life over the Indian Ocean at a longitude of 63 degrees east. Intelsat 604, previously named Intelsat VI F-4, was a communications satellite operated by Intelsat. It was to have been positioned in geostationary orbit at a longitude of 139° East, from where it was to have provided communications services to Asia and Oceania. Intelsat III F-1 was a communications satellite intended to be operated by Intelsat. Launched in 1969 it was intended for operations over the Pacific Ocean; however, it spent most of its service life over the Indian Ocean at a longitude of 63 degrees east. Originally formed as International Telecommunications Satellite Organization (INTELSAT), it was—from 1964 to 2001—an intergovernmental consortium owning and managing a constellation of communications satellites providing international broadcast services.. As of March 2011, Intelsat operates a fleet of 52 … [5], The third of eight Intelsat III satellites to be launched, Intelsat III F-3 was built by TRW. As of 2012, Intelsat 602 remains operational. [6] It was designed for 5 years of service life.[7]. The satellite had an estimated useful life of 5 years. Another 14 satellites, the Intelsat V-A and VI series, are under contract. The satellite carried 38 C-band and 10 K-band transponders, to provide telephone, TV and data services to large ground stations and small terminals. Launch Site: Cape Canaveral. Intelsat 605, previously named Intelsat VI F-5, was a communications satellite operated by Intelsat. Intelsat III F-3 was a geostationary communications satellite operated by Intelsat. Launched in 1990, it was the second of five Intelsat VI satellites to be launched. [3] [8], At the end of its service life, Intelsat III F-3 was raised into a higher orbit to reduce the probability of it colliding with an operational spacecraft. Intelsat II F-3, also known as Canary Bird was a communications satellite operated by Intelsat. The satellite had an estimated useful life of 5 years. The first of eight Intelsat III satellites to be launched, Intelsat III F-1 was built by TRW. [1] Lançamento. As of February 3, 2014 it remains in orbit, with a perigee of 39,935 kilometers (24,814 mi), an apogee of 41,521 kilometers (25,800 mi), inclination of 18.63 degrees and an orbital period of 28.25 hours. Intelsat III F-3 bija starpvalstu organizācijas Intelsat sakaru pavadonis. Geostationary satellite service began in 1965 with the launch of Intelsat I over the Atlantic region. The orbit data is extracted from the following two-line orbital elements, 1 2717U 67026A 20335.80187102 -.00000038 +00000-0 +00000-0 0 9990 2 2717 001.2013 315.2217 0019911 302.3723 094.1500 01.00276181103603 The launch of Intelsat III F-3 made use of a Delta M rocket flying from Launch Complex 17A at the Cape Canaveral Air Force Station. O satélite foi lançado ao espaço no dia 26 de julho de 1969, às 02:06:00 UTC, por meio de um veículo Delta M a partir da Estação da Força Aérea de Cabo Canaveral, na Flórida, EUA. It was a 293-kilogram (646 lb) spacecraft, with … Launched in 1966 it was intended for operations in geostationary orbit over the Pacific Ocean to provide a communications link between Australia and the United States, however a malfunction prevented the satellite from reaching its planned orbit. Intelsat III F-3 está disponível em 2 outras línguas. 2. Intelsat III F-3 is similar to these spaceflights: Intelsat III F-2, Intelsat III F-1, Intelsat III F-5 and more. Launched in 1997 it was operated in geostationary orbit at a longitude of 174 degrees west for around fourteen years. The spacecraft had a mass of 162 kilograms (357 lb) at launch, decreasing through expenditure of propellant to 86 kilograms (190 lb) by the …

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