KazEOSat 2
Remote sensing Earth observation satellite
| Mission type | Remote sensing |
|---|---|
| Operator | Kazakhstan Gharysh Sapary (KGS) |
| COSPAR ID | 2014-033A[1] |
| SATCAT no. | 40010 |
| Website | kazcosmos |
| Mission duration | 3 years |
| Spacecraft properties | |
| Bus | SSTL-150 |
| Manufacturer | EADS Astrium |
| Launch mass | ~177 kilograms (390 lb) |
| Dimensions | 700 by 800 by 900 millimetres (28 in × 31 in × 35 in) |
| Power | 150 watts |
| Start of mission | |
| Launch date | June 19, 2014, 19:11 (2014-06-19UTC19:11Z) UTC |
| Rocket | Dnepr |
| Launch site | Dombarovsky 370/13 |
| Contractor | Kosmotras |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-Synchronous |
| Perigee altitude | 611 kilometres (380 mi) |
| Apogee altitude | 636 kilometres (395 mi) |
| Inclination | 97.9 degrees |
| Period | 97.1 minutes |
| Epoch | 26 June 2014[2] |
KazEOSat is a remote sensing Earth observation satellite built for the Kazakhstan Gharysh Sapary under an agreement with EADS Astrium and SSTL, a satellite manufacturing companies in France and England, respectively. The earth observation satellite was designed and developed by EADS Astrium, and represent 11th launch of SSTL-150 bus, first launched in 2005.[3]
References
External links
Spaceflight portal
- KAzEOSat 2 launch announcement
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Orbital launches in 20142015 →
- GSAT-14
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- ARSAT-1, Intelsat 30
- Yaogan 22
- Ekspress AM6
- Chang'e 5-T1, 4M
- Shijian 11-08
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- Progress M-25M
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- Kondor-E No.2
- IPM
- Kosmos 2502
- Resurs-P No.2
- Yaogan 26
- Astra 2G
- Fengyun 2-08
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller.
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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