Lemur 1

USA

Spacecraft nº:

US spacecraft nº:


Launch data:

Designation 40044 / 14033AL
Launch date 19 June 2014 - 19:11 UT
Launch site Dombarovsky, LC-370/13
Launch vehicle  Dnepr
Mission Technology, Earth observation
Earth orbit:
Perigee / Apogee 617 x 704 km
Eccentricity 
Inclination  98.0°
Period 97.8 min

Launched together with: Deimos 2 - 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 - QB50P1 - QB50P2 - PACE - ANTELSAT - DTUSat 2 - Duchifat 1 - NanoSatC-Br 1 - PolyITAN 1 - AeroCube 6A - AeroCube 6B

Spacecraft data:

Prime manufacturer NanoSatisfi Inc. --> Spire
Platform CubeSat (3U)
Operator NanoSatisfi Inc. --> Spire
Mass at launch  4 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment visible light camera, infra-red camera
Solar array Solar cells
Stabilization  
Propulsion None
DC power  
Design lifetime  



Description:

Mission details:

External links:


Ref.: #7(JR699), #14, #228 - update: 04.12.14 Home