Ekspress-AM7: Difference between revisions
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Revision as of 00:14, 21 April 2015
| Mission type | Communications |
|---|---|
| Operator | RSCC |
| COSPAR ID | 2015-012A |
| SATCAT no. | 40505 |
| Mission duration | 15 years (planned) |
| Spacecraft properties | |
| Bus | Eurostar 3000 |
| Manufacturer | Airbus Defence and Space |
| Launch mass | 5,720 kilograms (12,610 lb)[1] |
| Start of mission | |
| Launch date | 18 March 2015, 22:05:00 UTC[2] |
| Rocket | Proton-M/Briz-M |
| Launch site | Baikonur 200/39 |
| Contractor | Khrunichev |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geosynchronous |
| Longitude | 40° East |
| Inclination | 0 degrees |
| Period | 24 hours |
| Epoch | Planned |
| Transponders | |
| Band | 24 C band 36 Ku band 2 L band |
Ekspress AM7 (Template:Lang-ru meaning Express AM7) is a Russian communications satellite operated by the State Company for Satellite Communications.
Astrium, which had become part of Airbus Defence and Space by the time of the satellite's launch, constructed Ekspress AM7, which was based on the Eurostar 3000 satellite bus.[3] The satellite has a mass of 5,720 kilograms (12,610 lb) and a planned operational lifespan of 15 years. The satellite carried 62 transponders: 24 operating in the C band of the electromagnetic spectrum, 36 in the Ku band and 2 in the L band. [1]
Khrunichev was contracted to launch Ekspress AM7, using a Proton-M/Briz-M rocket - the same configuration that had failed to deploy the similar Ekspress AM4 and Ekspress AM4R. The launch took place from Site 200/39 at the Baikonur Cosmodrome, at 22:05 UTC on 18 March 2015. The satellite was deployed into the planned geostationary transfer orbit.
References
- ^ a b "Express AM7". RSCC. Retrieved 19 March 2015.
- ^ Bergin, Chris. "Russian Proton-M launches with Ekspress-AM7 mission". NASASpaceflight.com. Retrieved 19 March 2015.
- ^ "Express AM4R and Express AM7". Airbus Defense and Space. Retrieved 19 March 2015.
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