Intelsat II F-3 explained

Intelsat II F-3
Mission Type:Communications
Operator:Intelsat
Cospar Id:1967-026A[1]
Satcat:2717
Mission Duration:3 years
Spacecraft Bus:HS-303A
Spacecraft Type:Intelsat II
Manufacturer:Hughes
Power:85 watts
Launch Date: UTC[2]
Launch Rocket:Delta E1
Launch Site:Cape Canaveral LC-17B
Launch Contractor:NASA
Deactivated:Early 1970s
Orbit Epoch:February 7, 2014, 14:16:27 UTC[3]
Orbit Reference:Geocentric
Orbit Regime:Geosynchronous
Orbit Periapsis:35716km (22,193miles)
Orbit Apoapsis:35892km (22,302miles)
Orbit Inclination:5.81 degrees
Orbit Period:23.94 hours
Orbit Longitude:15° west (1967-71, 1973)
35° west (1972)
Apsis:gee
Programme:Intelsat II
Previous Mission:Intelsat II F-2
Next Mission:Intelsat II F-4

Intelsat II F-3, also known as Canary Bird was a communications satellite operated by Intelsat. Launched in 1967 it was operated in geostationary orbit, spending most of its operational life at a longitude of 15 degrees west.

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. It carried two transponders, which were powered by body-mounted solar cells generating 85 watts of power.[4] The spacecraft had a mass of 162kg (357lb) at launch, decreasing through expenditure of propellant to 86kg (190lb) by the beginning of its operational life.

Intelsat II F-3 was launched atop a Delta E1 rocket flying from Launch Complex 17B at the Cape Canaveral Air Force Station. The launch took place at 01:30:12 on March 23, 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 15° west, over the Atlantic Ocean. It was briefly relocated to 35° west in 1972, but had returned to 15° west by the following year.[5]

It acquired the unofficial nickname Canary Bird because of the association of the mission with Maspalomas Station, the ground station which is located in the Canary Islands.[6]

As of February 7, 2014 the derelict Intelsat II F-3 was in an orbit with a perigee of 35716km (22,193miles), an apogee of 35892km (22,302miles), inclination of 5.81 degrees and an orbital period of 23.94 hours.[3]

Notes and References

  1. Web site: INTELSAT 2 F-3. National Space Science Data Center. February 8, 2014.
  2. Web site: Launch Log. Jonathan. McDowell. Jonathan's Space Page. February 8, 2014.
  3. Web site: INTELSAT 2-F3 Satellite details 1967-026A NORAD 2717. N2YO. February 7, 2014. February 8, 2014.
  4. Web site: Intelsat-2. Gunter. Krebs. Gunter's Space Page. February 8, 2014.
  5. Encyclopedia: Intelsat 2. https://web.archive.org/web/20020223093831/http://www.astronautix.com/craft/intlsat2.htm. dead. February 23, 2002. Mark. Wade. Encyclopedia Astronautica. February 8, 2014.
  6. Book: Dickson . Paul . A Dictionary of the Space Age. NASA/Johns Hopkins University Press . 11 February 2019 . Baltimore . 101 . 2009 .