| Mission type | Communications |
|---|---|
| Operator | Hispasat |
| COSPAR ID | 2004-031A |
| SATCATno. | 28393 |
| Mission duration | 15 years |
| Spacecraft properties | |
| Bus | Eurostar 3000 |
| Manufacturer | Astrium |
| Launch mass | 4,545 kilograms (10,020 lb) |
| Dimensions | 5,88 m x 2,4 m x 2,9 m (body) 36,10 m (solar arrays) |
| Power | 9,500 watts (EOL)[1] |
| Start of mission | |
| Launch date | 5 August 2004 (2004-08-05) |
| Rocket | Proton-MBriz-M |
| Launch site | Baikonur,Kazakhstan |
| End of mission | |
| Disposal | Graveyard orbit |
| Deactivated | 23 June 2017 (2017-06-24) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Transponders | |
| Band | C,Ku |
Amazonas 1 orHispasat 55W-1 was acommunications satellite based on theEurostar 3000 satellite bus and owned by satellites operatorHispasat, based inMadrid, Spain. It was launched on 5 August 2004, with a launch mass of 4,5 ton, on aProton-MBriz-M launcher to be located in the 61º Wgeostationary position.[2]
Amazonas 1 payloads were 36Ku bandtransponders that provided communications services in Europe andAmerica, and 27C band transponders that provided services in America. In 2013 it was relocated to the 36º W position and replaced byAmazonas 3.
In March 2016, Hispasat announced that Amazonas 1 would be renamed as Hispasat 55W-1. Finally, the satellite was moved to agraveyard orbit and deactivated on 23 June 2017.[3][4]
