Jcsat 13
Also called Jcsat 4B
General
| Designation | 38331 / 12023A |
| Launch date | 15 May 2012 |
| Country of origin | Japan |
| Mission | Telecommunications |
| Geostationary orbit | see below |
| Launch vehicle | Ariane VA206 |
To replace Jcsat 6
Location
| Begin | End | Position |
| L: 15 May 2012 | Jun 2012 | 127°E |
| Jul 2012 | 124°E, "Jcsat 4B" |
sat-index articles
Technical data
Lyngsat transponder loading
EIRP coverage (dBW)
Ku-band South East Asia
Specifications
| Prime contractor | Lockheed Martin |
| Platform | A2100AX |
| Mass at launch | 4528 kg |
| Mass in orbit | |
| Dimension | 6.0 x 3.3 x 2.6 m |
| Solar array | 27 m span |
| Stabilization | 3-axis |
| DC power | EOL: 11.9 kW |
| Design lifetime | 15 years |
Ku-band
| Main transponders | 44 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage |
Japan South-East Asia Hawaii + 2 steerable beams |
| EIRP max |
Japan:
56 dBW South-East Asia: 52 dBW Steerable: 51 dBW |
| G/T max | |
| Polarization |
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly