Deimos-2
| Mission type | Remote sensing |
|---|---|
| Operator | Deimos Space |
| COSPAR ID | 2014-033D[1] |
| Website |
www |
| Mission duration | 7 years |
| Spacecraft properties | |
| Bus | SI-300 |
| Manufacturer | Satrec Initiative |
| Launch mass | ~310 kilograms (680 lb) |
| Dimensions |
1,200 by 1,200 millimetres (47 in × 47 in) (Hexagonal) |
| Power | 330 watts |
| Start of mission | |
| Launch date | June 19, 2014, 19:11 UTC |
| Rocket | Dnepr |
| Launch site | Dombarovsky 370/13 |
| Contractor | Kosmotras |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-Synchronous |
| Perigee | 600 kilometres (370 mi) |
| Apogee | 600 kilometres (370 mi) |
| Inclination | 97.9 degrees |
| Main camera | |
| Name | DMAC |
| Wavelengths |
Pan: 420-720 nm MS1: 420-510 nm (Blue) MS2: 510-580 nm (Green) MS3: 600-720 nm (Red) MS4: 760-890 nm (Near Infrared) |
| Resolution |
0.75 metres (2 ft 6 in) (Pan) 5 metres (16 ft) (MS) |
Deimos-2 is a remote sensing Earth observation satellite built for Deimos Imaging under an agreement with Satrec Initiative, a satellite manufacturing company in South Korea. The earth observation satellite was designed and developed by Satrec Initiative, and represent nearly exact copy of DubaiSat-2 launched in 2013, except for the larger battery pack intended to last for at least 7 years.[2]
See also
- Oriondata Internacional: reseller of Deimos-1, Deimos-2 in Chile and others countries in Latin America
References
- ↑ "Deimos 2 Gunters space page". Retrieved June 24, 2014.
- ↑ http://www.gsdi.org/gsdiconf/gsdi14/slides/4.2Deimos.pdf
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