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 Launch  





2 References  














Intelsat VA F-10






Deutsch
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 VA F-10 → Intelsat 510
Mission typeCommunication
OperatorIntelsat
COSPAR ID1985-025A [1]
SATCAT no.15629
Mission duration9 years (planned)
Spacecraft properties
BusIntelsat-VA
ManufacturerFord Aerospace
Launch mass2013 kg
Dry mass1098 kg [2]
Power1800 watts
Start of mission
Launch date22 March 1985, 23:55:00 UTC [3]
RocketAtlas G (AC-63)
Launch siteCCAFS, LC-36B
ContractorGeneral Dynamics
End of mission
DisposalGraveyard orbit
DeactivatedJuly 1999
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Epoch22 March 1985
Transponders
Band26C-Band
6Ku-band
Intelsat V
 

Intelsat 510, previously named Intelsat VA F-10, was a communications satellite operated by Intelsat. Launched in 1985, it was the tenth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat-VA satellite bus. Intelsat VA F-10 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.

Launch

[edit]

The satellite was successfully launched into space on 22 March 1985, at 23:55:00 UTC, by means of an Atlas-Centaur G vehicle from the Cape Canaveral Air Force Station, Florida, United States. It had a launch mass of 2013 kg. The Intelsat 510 was equipped with 6 Ku-band transponders more 26 C-band transponders for 15,000 audio circuits and 2 TV channels.

References

[edit]
  1. ^ "Display: Intelsat 5A F-10 1985-025A". NASA. 14 May 2020. Retrieved 29 June 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  • ^ "Intelsat-5A". Gunter's Space Page. Retrieved 23 April 2017.
  • ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 23 April 2017.
  • t
  • e

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Intelsat_VA_F-10&oldid=1192920932"

    Categories: 
    Spacecraft launched in 1985
    Intelsat satellites
    SES satellites
    Spacecraft stubs
    Hidden categories: 
    Source attribution
    Use British English from June 2020
    Use dmy dates from June 2020
    All stub articles
     



    This page was last edited on 1 January 2024, at 02:11 (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