Official name VENESAT-1
Alternative name Simon Bolivar
Cospar ID 2008-055A
Norad ID 33414
Launch date 2008-10-29
Launch site XSC
Launch vehicle CZ-3B/G2
Country/Organization Venezuela
Type application Communication
Operator Ministry of Science and Technology of Venezuela
RCS size LARGE
Decay date ON ORBIT
Period (min) 1450.61
Inclination (deg) 3.76
Perigee (km) 35813
Apogee (km) 36327
Eccentricity 0.00712503465483782
Mean motion (revs. per day) 0.992685835613983
Semi-Major axis (km) 42448.135
Raan (deg) 82.22
Arg of perigee (deg) 174.2483
Shape Box + 2 Pan
Mass (kg) 5100
Height (m) 3.6
Width (m) 2.4
Depth (m) 2.4
Span (m^2) 15.5
Lifetime 15 years
Contractors CAST
Equipment 14 C-band, 12 Ku-band and 2 Ka-band transponders
Configuration DFH-4 Bus
Power 2 deployable solar arrays, batteries

Under an agreement signed in November 2005, the China Great Wall Industry Corp was contracted to design, manufacture, test and put into orbit the VENESAT-1 for Venezuela.

The satellite will help Venezuela develop its telecommunications, film and TV industries, culture and education. The planned telecommunications satellite will blast off from Xichang Satellite Launch Centre in Southwest China atop a CZ-3B/G2 rocket. The satellite, designed with a mission life of 15 years, was constructed by the China Academy of Space Technology, based on the country's DFH-4 Bus, China's new-generation telecommunications satellite platform. The satellite is also called the "Simon Bolivar Satellite," named after the Caracas-born South American independence hero, the Liberator of Five Republics, according to Tenorio.

The satellite was launched in 2008.

On 13 March 2020 a series of maneuvers left it tumbling in an unusable orbit, with a lowest point 50 km and the highest point 525 km above the geosynchronous arc. Possibly the mishap occured while moving the satellite into a proper graveyard orbit. An issue with the solar arrays has been confirmed.

Satellite COSPAR Date LS Launch Vehicle Remarks
VENESAT-1 2008-055A 2008-10-29 XSC CZ-3B/G2