A | B | C | D | E | F | G | H | CH | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | 0 | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9
Mission type | Communications |
---|---|
Operator | Intelsat |
COSPAR ID | 1967-001A |
SATCAT no. | 2639 |
Mission duration | 3 years |
Spacecraft properties | |
Spacecraft type | Intelsat II |
Bus | HS-303A |
Manufacturer | Hughes |
Launch mass | 162 kilograms (357 lb) |
BOL mass | 86 kilograms (190 lb) |
Power | 85 watts |
Start of mission | |
Launch date | January 11, 1967, 10:55:00[1] | UTC
Rocket | Delta E1 |
Launch site | Cape Canaveral LC-17B |
End of mission | |
Deactivated | c.1969[2] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geosynchronous |
Longitude | 174° 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]
References
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved February 8, 2014.
- ^ a b c Wade, Mark. "Intelsat 2". Encyclopedia Astronautica. Archived from the original on December 28, 2016. Retrieved September 22, 2021.
- ^ a b "INTELSAT 2-F2 Satellite details 1967-001A NORAD 2639". N2YO. February 4, 2014. Retrieved February 8, 2014.
- ^ Krebs, Gunter. "Intelsat-2". Gunter's Space Page. Retrieved February 8, 2014.
- ^ "INTELSAT 2 F-2". National Space Science Data Center. Retrieved February 8, 2014.
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