Yahsat 1B
General
| Designation | 38245 / 12016A |
| Launch date | 23 Apr 2012 |
| Country of origin | United Arab Emirates |
| Mission | Telecommunications |
| Geostationary orbit | 47.5°E |
| Launch vehicle | Proton |
Initially planned for launch in 2010. Mostly identical to Yahsat 1A
sat-index articles
Technical data
Lyngsat transponder loading
Specifications
| Prime contractor | EADS Astrium & Thales Alenia Space |
| Platform | Eurostar-3000 |
| Mass at launch | 5965 kg |
| Dry mass | |
| Dimension | 5.5 x 2.1 x 2.3 m |
| Solar array | |
| Stabilization | 3-axis |
| DC power | 9.7 kW |
| Design lifetime | 15 years |
Ka-band government
| Main transponders | 14 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | |
| EIRP max | |
| G/T max | |
| Polarization |
Ka-band commercial
| Main transponders | 60 spot beams |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | |
| EIRP max | |
| G/T max | |
| Polarization |
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V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly