Intelsat II F-2

Last updated
Intelsat II F-2
Mission type Communications
Operator Intelsat
COSPAR ID 1967-001A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 2639
Mission duration3 years
Spacecraft properties
Spacecraft type Intelsat II
Bus HS-303A
Manufacturer Hughes
Launch mass162 kilograms (357 lb)
BOL mass 86 kilograms (190 lb)
Power85 watts
Start of mission
Launch dateJanuary 11, 1967, 10:55:00 (1967-01-11UTC10:55Z) UTC [1]
Rocket Delta E1
Launch site Cape Canaveral LC-17B
End of mission
Deactivatedc.1969 (1970) [2]
Orbital parameters
Reference system Geocentric
Regime Geosynchronous
Longitude174° east [2]
Perigee altitude 35,748 kilometers (22,213 mi)
Apogee altitude 35,845 kilometers (22,273 mi)
Inclination 6.80 degrees
Period 23.93 hours
Epoch February 4, 2014, 11:35:30 UTC [3]
 

Intelsat II F-2, also known as Lani Bird, was a communications satellite operated by Intelsat. Launched in 1967, it was operated in geostationary orbit at a longitude of 174 degrees east until 1969.

The second of four Intelsat II satellites to be launched, Intelsat II F-2 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 162 kilograms (357 lb) at launch, decreasing to 86 kilograms (190 lb) by the beginning of its operational life.

Intelsat II F-2 was launched atop a Delta E1 rocket flying from Launch Complex 17B at the Cape Canaveral Air Force Station. The launch took place at 10:55:00 on January 11, 1967, with the spacecraft entering a geosynchronous transfer orbit. It fired an SVM-1 apogee motor to place itself into its operational geostationary orbit, arriving on-station at 174° East on February 4, 1967. [5] The satellite achieved around two years of operation at that slot before failing in 1969. [2]

As of February 4, 2014, Intelsat II F-2 was in an orbit with a perigee of 35,748 kilometers (22,213 mi), an apogee of 35,845 kilometers (22,273 mi), inclination of 6.80 degrees and an orbital period of 23.93 hours. [3]

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References

  1. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved February 8, 2014.
  2. 1 2 3 Wade, Mark. "Intelsat 2". Encyclopedia Astronautica. Archived from the original on December 28, 2016. Retrieved September 22, 2021.
  3. 1 2 "INTELSAT 2-F2 Satellite details 1967-001A NORAD 2639". N2YO. February 4, 2014. Retrieved February 8, 2014.
  4. Krebs, Gunter. "Intelsat-2". Gunter's Space Page. Retrieved February 8, 2014.
  5. "INTELSAT 2 F-2". National Space Science Data Center. Retrieved February 8, 2014.