About: Intelsat III F-3

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Intelsat III F-3 was a geostationary communications satellite 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.

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:Abstraction100002137 yago:Act100030358 yago:Action100037396 yago:Change100191142 yago:Event100029378 yago:Journey100306426 yago:Motion100279835 yago:PsychologicalFeature100023100 yago:YagoPermanentlyLocatedEntity event space mission yago:Spaceflight100313502 yago:Travel100295701 yago:Voyage100312553 ArtificialSatellite
rdfs:label	Intelsat III F-3 (en) Intelsat III F-3 (pt)
rdfs:comment	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. O satélite tinha uma vida útil estimada de 5 anos. (pt) Intelsat III F-3 was a geostationary communications satellite 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. (en)
foaf:name	Intelsat III F-3 (en)
name	Intelsat III F-3 (en)
dcterms:subject	Spacecraft launched in 1969 Intelsat satellites
Wikipage page ID	41890498 (xsd:integer)
Wikipage revision ID	1084019662 (xsd:integer)
Link from a Wikipage to another Wikipage	Cape Canaveral Air Force Station Cape Canaveral Air Force Station Space Launch Complex 17 Apsis Geocentric orbit Geostationary orbit Geosynchronous orbit NASA Communications satellite Delta M Orbital period TRW Inc. Spacecraft launched in 1969 Transponder Pacific Ocean Graveyard orbit Intelsat satellites Apogee motor Indian Ocean Intelsat Intelsat III F-2 Intelsat III F-4 Orbital inclination Geosynchronous transfer orbit dbr:Intelsat_III dbr:SVM-2
sameAs	Intelsat III F-3 Intelsat III F-3 Intelsat III F-3 Intelsat III F-3 Intelsat III F-3
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Use_American_English dbt:Use_mdy_dates dbt:End-date dbt:Start-date dbt:Orbital_launches_in_1969 dbt:Intelsat
apsis	gee (en)
auto	all (en)
COSPAR ID	1969 (xsd:integer)
image caption	Intelsat III F-3. (en)
image size	180 (xsd:integer)
launch contractor	NASA
launch date	0001-02-06 (xsd:gMonthDay)
launch rocket	Delta M
launch site	Cape Canaveral Air Force Station Cape Canaveral Air Force Station Space Launch Complex 17
manufacturer	TRW Inc.
mission duration	1.57788E8 (second)
mission type	Communications satellite
next mission	Intelsat III F-4
operator	Intelsat
orbit inclination	18.330000 (xsd:double)
orbit period	101729.4 (second)
orbit reference	Geocentric orbit
orbit regime	Geosynchronous orbit (Now Graveyard) (en)
power	183 (xsd:integer)
previous mission	Intelsat III F-2
programme	Intelsat III (en)
SATCAT	3674 (xsd:integer)
spacecraft type	dbr:Intelsat_III
has abstract	Intelsat III F-3 was a geostationary communications satellite 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. The third of eight satellites to be launched, Intelsat III F-3 was built by TRW. It was a 293-kilogram (646 lb) spacecraft, with its mass reducing to 151 kilograms (333 lb) by entry into service as it burned propellant to reach its final orbit. The satellite carried an apogee motor for propulsion and was equipped with two transponders powered by body-mounted solar cells generating 183 watts of power. It was designed for 5 years of service life. 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. The launch, which was conducted by NASA, took place at 00:39:00 UTC on February 6, 1969, with the spacecraft entering a geosynchronous transfer orbit. Shortly after launch, Intelsat III F-3 fired its apogee motor to achieve geostationary orbit. Intended to be operated over the Pacific Ocean at a longitude of 174° east, Intelsat III F-3 was moved to the less important Indian Ocean slot at 63° east after only three months in orbit due to concerns regarding its reliability. The satellite was only regarded as partially operable; however, it remained in service until April 1979, before being decommissioned in December of that year. 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. 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. (en) 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. O satélite tinha uma vida útil estimada de 5 anos. (pt)
deactivated	1979-12-14 (xsd:date)
disposal type	Decommissioned (en)

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