Viking 1

USA


Spacecraft n°:

USA satellite n°:

Also called: Viking 1 Orbiter

Launch data:

Designation  08108 / 75075A
Launch date  20 Aug 1975 - 21:22 UT
Launch site CC, LC-41
Launch vehicle  Titan-3E Centaur-D1T (#23E-4/TC-4)
Mission  Mars lander
Satellite type 
Heliocentric orbit
Perihelion / Aphelion  1.003 x 1.672 AU
Eccentricity 0.250
Inclination 4.48 deg
Period  565 days
Mars orbit on 1976 Jun 19:
Perihelion / Aphelion  1500 x 50600 km
Eccentricity 0.834
Inclination 37.8? deg
Period  2544 min
Mars orbit on 1979 Jul 20:
Perihelion / Aphelion  357 x 33943 km
Eccentricity 0.817
Inclination 39.9 deg
Period  1487 min
Mars orbit on 1980 Aug 08:
Perihelion / Aphelion  320 x 56000 km
Eccentricity 0.760
Inclination 40? deg
Period  2830 min

Viking 1 Orbiter



Spacecraft data:

Prime contractor  
Operator 
Platform  
Mass at launch  2325 kg (full)
Dry Mass  kg
Basic shape  Octagonal box + 4 vanes
Dimension  3.3 high - 1.8 wide - 1.5 deep
Solar array  
Stabilization  
DC power  
Design lifetime  44 years? - In Mars orbit

Viking lander model


Mission details:


Ref.: #1, #7(JR326,327,664), #81, #206 - update: 12.08.12 Home