Sentinel-1A

ESA

Spacecraft nº:

ESA spacecraft nº: 86


Launch data:

Designation 39634 / 14016A
Launch date 03 April 2014 - 21:02 UT
Launch site CSG, ELS
Launch vehicle  Soyuz-STA / Fregat-M (Soyuz-2-1A?)
Mission Earth Observing (Radar)
Earth orbit:
Perigee / Apogee 702 x 704 km
Eccentricity 
Inclination 98.2 °
Period 98.7 min


Spacecraft data:

Prime manufacturer Thales Alenia Space
Platform Prima Bus
Operator ESA
Mass at launch  2280 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment C-band synthetic aperture radar (SAR)
Solar array 2 deployable solar arrays
Stabilization  
Propulsion 
DC power  
Design lifetime  7 yrs



Description:

Mission details:

External links:


Ref.: #7(JR696), #14, #228 - update: 02.12.14 Home