Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 References  














Intelsat V F-8






Português
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Intelsat V F-7 → Intelsat 507
Mission typeCommunication
OperatorIntelsat
COSPAR ID1984-023A[1]
SATCAT no.14786[2]
Mission duration13 years
Spacecraft properties
BusIntelsat-V bus
ManufacturerFord Aerospace
Launch mass1,928.2 kilograms (4,251 lb)[3]
BOL mass1,012 kilograms (2,231 lb)[3]
Start of mission
Launch dateMarch 05, 1984, 00:50:03 (1984-03-05UTC00:50:03Z) UTC[4]
RocketAriane 1[5]
Launch siteKourou ELA-1[5]
End of mission
DisposalDecommissioned
DeactivatedAugust, 1996 (1996-08-13)
Orbital parameters
Reference systemGeocentric[2]
RegimeGeostationary[2]
Longitude180° W (original position)
33° E (current position)[2]
Semi-major axis43,021 kilometers (26,732 mi)[2]
Perigee altitude36,580.8 kilometers (22,730.3 mi)[2]
Apogee altitude36,720.2 kilometers (22,816.9 mi)[2]
Inclination16.0 degrees[2]
Period1,480.1 minutes[2]
EpochApril 23, 2017[2]
Transponders
Band21C-band
4Ku band
Intelsat V
 

Intelsat 508, previously named Intelsat V F-8, was a communications satellite operated by Intelsat. Launched in 1984, it was the eighth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat-V satellite bus. Intelsat V F-8 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.

The satellite was successfully launched into space on October 19, 1983, at 00:45 UTC, by means of an Ariane 1 vehicle from the Guiana Space Centre, Kourou, French Guiana. It had a launch mass of 1,928 kg.[6] The Intelsat V F-8 was equipped with 4 Ku-band transponders more 21 C-band transponders for 12,000 audio circuits and 2 TV channels.

References

[edit]
  1. ^ "INTELSAT 5 F-8". National Space Science Data Center. Retrieved April 23, 2017.
  • ^ a b c d e f g h i j "Intelsat 508". N2yo.com. Retrieved April 23, 2017.
  • ^ a b "Intelsat-5". Gunter's Space Page. Retrieved April 23, 2017.
  • ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved April 23, 2017.
  • ^ a b Wade, Mark. "Launch Log". Astronautix. Archived from the original on December 27, 2016. Retrieved April 23, 2017.
  • ^ "INTELSAT 508". TSE. Retrieved April 23, 2017.

  • t
  • e

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Intelsat_V_F-8&oldid=1173866741"

    Categories: 
    Spacecraft launched in 1984
    Intelsat satellites
    Spacecraft stubs
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    All stub articles
     



    This page was last edited on 4 September 2023, at 22:21 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki