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Intelsat 805

0°00′N 168°58′W / 0°N 168.97°W / 0; -168.97

Intelsat 805
Mission typeCommunications
OperatorIntelsat
COSPAR ID1998-037A
SATCAT no.25371
Mission duration14 years (planned)
Spacecraft properties
Spacecraft typeAS-7000
ManufacturerLockheed Martin
Launch mass3,524 kilograms (7,769 lb)
Start of mission
Launch dateJune 18, 1998, 22:48 (1998-06-18UTC22:48Z) UTC[1]
RocketAtlas IIAS AC-153
Launch siteCape Canaveral SLC-36A
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
Now supersynchronous
Semi-major axis42,164 kilometres (26,199 mi)
Perigee altitude35,778.0 kilometres (22,231.4 mi)
Apogee altitude35,809.0 kilometres (22,250.7 mi)
Inclination
Period1,436.1 minutes
EpochMay 6, 2017[2]
Transponders
Band28 C Band, 3 Ku band
Coverage areaAmericas, Europe
Intelsat 8
 

Intelsat 805 is a communications satellite operated by Intelsat. Launched in 1998, it was operated in geostationary orbit at a longitude of 55.5 degrees west for around 14 years.

Launch edit

The launch of Intelsat 805 made use of an Atlas II rocket flying from Cape Canaveral Air Force Station, Florida, United States. The launch took place at 22:48 UTC on June 18, 1998, with the spacecraft entering a geosynchronous transfer orbit. Intelsat 805 subsequently fired its apogee motor to achieve geostationary orbit.

Technical details edit

References edit

  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved May 5, 2017.
  2. ^ "INTELSAT 805". N2YO. Retrieved May 6, 2017.


intelsat, mission, typecommunicationsoperatorintelsatcospar, id1998, 037asatcat, 25371mission, duration14, years, planned, spacecraft, propertiesspacecraft, typeas, 7000manufacturerlockheed, martinlaunch, mass3, kilograms, start, missionlaunch, datejune, 1998,. 0 00 N 168 58 W 0 N 168 97 W 0 168 97 Intelsat 805Mission typeCommunicationsOperatorIntelsatCOSPAR ID1998 037ASATCAT no 25371Mission duration14 years planned Spacecraft propertiesSpacecraft typeAS 7000ManufacturerLockheed MartinLaunch mass3 524 kilograms 7 769 lb Start of missionLaunch dateJune 18 1998 22 48 1998 06 18UTC22 48Z UTC 1 RocketAtlas IIAS AC 153Launch siteCape Canaveral SLC 36AOrbital parametersReference systemGeocentricRegimeGeostationaryNow supersynchronousSemi major axis42 164 kilometres 26 199 mi Perigee altitude35 778 0 kilometres 22 231 4 mi Apogee altitude35 809 0 kilometres 22 250 7 mi Inclination0 Period1 436 1 minutesEpochMay 6 2017 2 TranspondersBand28 C Band 3 Ku bandCoverage areaAmericas EuropeIntelsat 8 Intelsat 804Intelsat 806 Intelsat 805 is a communications satellite operated by Intelsat Launched in 1998 it was operated in geostationary orbit at a longitude of 55 5 degrees west for around 14 years Launch editThe launch of Intelsat 805 made use of an Atlas II rocket flying from Cape Canaveral Air Force Station Florida United States The launch took place at 22 48 UTC on June 18 1998 with the spacecraft entering a geosynchronous transfer orbit Intelsat 805 subsequently fired its apogee motor to achieve geostationary orbit Technical details editC Band slot chartSlot Uplink GHz Downlink GHz Hemi A Hemi B Bandwidth MHz 7 6 467 3 442 13 A 23 A 366 6 507 3 442 12 B 22 B 365 6 547 3 482 12 A 22 A 364 6 587 3 562 11 B 21 B 363 6 627 3 602 11 A 21 A 36 1 5 908 3 683 10 A 20 A 361 2 5 970 3 745 11 21 723 4 6 050 3 825 12 22 725 6 6 130 3 905 13 23 727 8 6 220 3 995 14 24 729 6 280 4 055 15 25 3610 6 320 4 095 16 26 3611 6 360 4 135 17 27 3612 6 4025 4 1775 18 28 41Ku band slot chartSlot Uplink GHz Polariztion H Downlink GHz Polarization V Spot 1 Bandwidth MHz 1 2 14 0425 12 5475 361 773 4 14 125 12 630 362 725 6 14 205 12 701 363 72 nbsp Spaceflight portalReferences edit McDowell Jonathan Launch Log Jonathan s Space Page Retrieved May 5 2017 INTELSAT 805 N2YO Retrieved May 6 2017 nbsp This article about one or more spacecraft of the United States is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title Intelsat 805 amp oldid 1182807377, wikipedia, wiki, book, books, library,

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