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- Intelsat_II_F-4 abstract "Intelsat II F-4 was a communications satellite operated by Intelsat. Launched in 1967 it was operated in geostationary orbit at a longitude of 176 degrees east and later 166 degrees west.The fourth and last Intelsat II satellite to be launched, Intelsat II F-4 was built by Hughes Aircraft around the HS-303A satellite bus. It carried two transponders, which were powered by body-mounted solar cells generating 85 watts of power. The spacecraft had a mass of 162 kilograms (357 lb) at launch, decreasing through expenditure of propellant to 86 kilograms (190 lb) by the beginning of its operational life.Intelsat II F-4 was launched atop a Delta E1 rocket flying from Launch Complex 17B at the Cape Canaveral Air Force Station. The launch took place at 00:45:00 UTC on September 28, 1967, with the spacecraft entering a geosynchronous transfer orbit. It fired an SVM-1 apogee motor to place itself into its operational geostationary orbit. The spacecraft was operated at a longitude of 176° east until 1970, before being moved to 166° west. In total the satellite remained in service for around three and a half years.As of February 8, 2014 the derelict Intelsat II F-4 was in an orbit with a perigee of 35,742 kilometers (22,209 mi), an apogee of 35,886 kilometers (22,299 mi), inclination of 6.00 degrees and an orbital period of 23.95 hours.".
- Intelsat_II_F-4 cosparId "1967-094A".
- Intelsat_II_F-4 wikiPageID "41885663".
- Intelsat_II_F-4 wikiPageLength "4723".
- Intelsat_II_F-4 wikiPageOutDegree "33".
- Intelsat_II_F-4 wikiPageRevisionID "682866380".
- Intelsat_II_F-4 wikiPageWikiLink Apogee_kick_motor.
- Intelsat_II_F-4 wikiPageWikiLink Apsis.
- Intelsat_II_F-4 wikiPageWikiLink Cape_Canaveral_Air_Force_Station.
- Intelsat_II_F-4 wikiPageWikiLink Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17.
- Intelsat_II_F-4 wikiPageWikiLink Category:Hughes_aircraft.
- Intelsat_II_F-4 wikiPageWikiLink Category:Intelsat_satellites.
- Intelsat_II_F-4 wikiPageWikiLink Category:Spacecraft_launched_in_1967.
- Intelsat_II_F-4 wikiPageWikiLink Communications_satellite.
- Intelsat_II_F-4 wikiPageWikiLink Delta_E.
- Intelsat_II_F-4 wikiPageWikiLink Geocentric_orbit.
- Intelsat_II_F-4 wikiPageWikiLink Geostationary_orbit.
- Intelsat_II_F-4 wikiPageWikiLink Geostationary_transfer_orbit.
- Intelsat_II_F-4 wikiPageWikiLink Geosynchronous_orbit.
- Intelsat_II_F-4 wikiPageWikiLink HS-303A.
- Intelsat_II_F-4 wikiPageWikiLink Hughes_Aircraft_Company.
- Intelsat_II_F-4 wikiPageWikiLink Intelsat.
- Intelsat_II_F-4 wikiPageWikiLink Intelsat_II.
- Intelsat_II_F-4 wikiPageWikiLink NASA.
- Intelsat_II_F-4 wikiPageWikiLink Orbital_inclination.
- Intelsat_II_F-4 wikiPageWikiLink Orbital_period.
- Intelsat_II_F-4 wikiPageWikiLink SVM-1.
- Intelsat_II_F-4 wikiPageWikiLink Satellite_bus.
- Intelsat_II_F-4 wikiPageWikiLink Transponder.
- Intelsat_II_F-4 wikiPageWikiLinkText "Intelsat II F-4".
- Intelsat_II_F-4 apsis "gee".
- Intelsat_II_F-4 cosparId "1967".
- Intelsat_II_F-4 deactivated "c.".
- Intelsat_II_F-4 launchContractor NASA.
- Intelsat_II_F-4 launchDate "--09-28".
- Intelsat_II_F-4 launchRocket Delta_E.
- Intelsat_II_F-4 launchSite Cape_Canaveral_Air_Force_Station.
- Intelsat_II_F-4 launchSite Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17.
- Intelsat_II_F-4 manufacturer Hughes_Aircraft_Company.
- Intelsat_II_F-4 missionDuration "9.46728E7".
- Intelsat_II_F-4 missionDuration "years achieved".
- Intelsat_II_F-4 missionType Communications_satellite.
- Intelsat_II_F-4 name "Intelsat II F-4".
- Intelsat_II_F-4 operator Intelsat.
- Intelsat_II_F-4 orbitEpoch "--02-08".
- Intelsat_II_F-4 orbitInclination "6".
- Intelsat_II_F-4 orbitLongitude "166".
- Intelsat_II_F-4 orbitLongitude "176".
- Intelsat_II_F-4 orbitPeriod "86220.0".
- Intelsat_II_F-4 orbitReference Geocentric_orbit.
- Intelsat_II_F-4 orbitRegime Geosynchronous_orbit.
- Intelsat_II_F-4 power "85".
- Intelsat_II_F-4 satcat "2969".
- Intelsat_II_F-4 spacecraftBus HS-303A.
- Intelsat_II_F-4 spacecraftType Intelsat_II.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Convert.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:End-date.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Frac.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Infobox_spaceflight.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Intelsat.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Orbital_launches_in_1967.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Reflist.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Start-date.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Use_American_English.
- Intelsat_II_F-4 wikiPageUsesTemplate Template:Use_mdy_dates.
- Intelsat_II_F-4 subject Category:Hughes_aircraft.
- Intelsat_II_F-4 subject Category:Intelsat_satellites.
- Intelsat_II_F-4 subject Category:Spacecraft_launched_in_1967.
- Intelsat_II_F-4 hypernym Satellite.
- Intelsat_II_F-4 type ArtificialSatellite.
- Intelsat_II_F-4 type CelestialBody.
- Intelsat_II_F-4 type Place.
- Intelsat_II_F-4 type Satellite.
- Intelsat_II_F-4 type Location.
- Intelsat_II_F-4 type Place.
- Intelsat_II_F-4 type Thing.
- Intelsat_II_F-4 comment "Intelsat II F-4 was a communications satellite operated by Intelsat. Launched in 1967 it was operated in geostationary orbit at a longitude of 176 degrees east and later 166 degrees west.The fourth and last Intelsat II satellite to be launched, Intelsat II F-4 was built by Hughes Aircraft around the HS-303A satellite bus. It carried two transponders, which were powered by body-mounted solar cells generating 85 watts of power.".
- Intelsat_II_F-4 label "Intelsat II F-4".
- Intelsat_II_F-4 sameAs Q14771250.
- Intelsat_II_F-4 sameAs Intelsat_II_F-4.
- Intelsat_II_F-4 sameAs m.0_ql0gt.
- Intelsat_II_F-4 sameAs Q14771250.
- Intelsat_II_F-4 wasDerivedFrom Intelsat_II_F-4?oldid=682866380.
- Intelsat_II_F-4 isPrimaryTopicOf Intelsat_II_F-4.