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Names | Экспрeсс-А1 Express-A1 Ekspress-6A No.1 |
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Mission type | Communication |
Operator | Russian Satellite Communications Company (RSCC) |
Website | https://eng.rscc.ru/ |
Mission duration | 7 years (planned) Failed to orbit |
Spacecraft properties | |
Spacecraft | Ekspress-A1 |
Spacecraft type | KAUR |
Bus | MSS-2500-GSO |
Manufacturer | NPO PM (bus) Alcatel Space (payload) |
Launch mass | 2,600 kg (5,700 lb) |
Power | 2540 watts |
Start of mission | |
Launch date | 27 October 1999, 16:16:00 UTC |
Rocket | Proton-K / DM-2 |
Launch site | Baikonur, Site 200/39 |
Contractor | Khrunichev State Research and Production Space Center |
Entered service | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit (planned) [1] |
Regime | Geostationary orbit |
Longitude | 11° West |
Transponders | |
Band | 17transponders: 12C-band 5Ku-band |
Coverage area | Russia |
Ekspress-A1 (Russian: Экспрeсс-А1 meaning Express-A1), also designated Ekspress-6A No.1, is a Russian communications satellite which is operated by Russian Satellite Communications Company (RSCC).
It was constructed by NPO Prikladnoi Mekhaniki (ISS Reshetnev) and Alcatel Space and is based on the MSS-2500-GSO satellite bus. It is equipped with seventeen transponders.
The satellite was launched at Baikonur CosmodromeatSite 200/39 on 27 October 1999, at 16:16:00 UTC. The launch was made by Khrunichev State Research and Production Space Center, and a Proton-K / DM-2 launch vehicle was used.[1] It is part of the Ekspress satellite constellation.
The Russian Ekspress-A1 communications satellite was launched in October 1999 but the Proton-K launch vehicle failed early in flight, during second stage burn. This is the second failure of the 8K82K Proton-K in 1999.[2]
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). |
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