Deimos 2

Spain

Spacecraft nº:

Spanish spacecraft nº: 19


Launch data:

Designation 40013 / 14033D
Launch date 19 June 2014 - 19:11 UT
Launch site Dombarovsky, LC-370/13
Launch vehicle  Dnepr
Mission Earth observation, imaging
Sun-synchronous Earth orbit:
Perigee / Apogee 624 x 628 km
Eccentricity 
Inclination  98.0°
Period 97.1 min

Launched together with: KazEOSat 2 - TabletSat-Aurora - BugSat 1 - SaudiSat 4 - Hodoyoshi 3 - Hodoyoshi 4 - AprizeSat 9 - AprizeSat 10 - UniSat 6 - BRITE-CA 1 - BRITE-CA 2 - Perseus-M 1 - Perseus-M 2 - Flock-1c 1-11 - POPSAT-HIP 1 - Tigrisat - Lemur 1 - QB50P1 - QB50P2 - PACE - ANTELSAT - DTUSat 2 - Duchifat 1 - NanoSatC-Br 1 - PolyITAN 1 - AeroCube 6A - AeroCube 6B

Spacecraft data:

Prime manufacturer Satrec Initiative (SATRECI)
Platform SI-300 bus
Operator Deimos
Mass at launch  ~300 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment EOS-D camera
Solar array 4 deployable fixed solar arrays
Stabilization  
Propulsion Hall Effect Propulsion System (HEPS)
DC power  
Design lifetime  



Description:

Mission details:

External links:


Ref.: #7(JR699), #14, #228, #242 - update: 03.12.14 Home