Engineering:Ekspress AM6
From HandWiki
Mission type | Communications |
---|---|
Operator | FGUP |
COSPAR ID | 2014-064A |
SATCAT no. | 40277 |
Mission duration | 15 years planned |
Spacecraft properties | |
Bus | Ekspress-2000 |
Manufacturer | ISS Reshetnev MDA Corporation |
Launch mass | 3,358 kilograms (7,403 lb) |
Start of mission | |
Launch date | 21 October 2014, 15:09:32[1] | UTC
Rocket | Proton-M/Briz-M |
Launch site | Baikonur 81/24 |
Contractor | Khrunichev |
Orbital parameters | |
Reference system | Geocentric |
Longitude | 53° East |
Perigee altitude | 35,774 kilometres (22,229 mi)[2] |
Apogee altitude | 35,799 kilometres (22,244 mi)[2] |
Inclination | 0.36 degrees[2] |
Period | 1436.1 minutes[2] |
Epoch | 18 March 2015, 16:26:01 UTC[2] |
Transponders | |
Band | 30 C band 40 Ku band 12 Ka band 2 L band |
Ekspress-AM6 (Russian: Экспресс АМ6) is a Russia n communications satellite which was launched in 2014. The satellite has replaced the older Ekspress-AM22, at 53° East. Part of the Ekspress series of geostationary communications satellites, it is owned and operated by the Russian State Company for Satellite Communications.
The satellite has 30 C-band, 40 Ku-band, 12 Ka-band and 2 L-band transponders.
List of providers
Company | Market | Website |
---|---|---|
RSCC | Russia and CIS | www.rscc.ru |
Wide Network Solutions | Middle East and Europe | www.widenetworks.net |
References
- ↑ Bergin, Chris (21 October 2014). "Russian Proton-M launches Ekspress-AM6 satellite – orbit unclear". http://www.nasaspaceflight.com/2014/10/russian-proton-m-ekspress-am6-mission/. Retrieved 19 March 2015.
- ↑ 2.0 2.1 2.2 2.3 2.4 "EXPRESS-AM6 Satellite details 2014-064A NORAD 40277". N2YO. 19 March 2015. http://www.n2yo.com/satellite/?s=39487. Retrieved 19 March 2015.