Names | Simón Bolívar |
---|---|
Mission type | Communication |
Operator | ABAE[1] |
COSPAR ID | 2008-055A |
SATCAT no. | 33414 |
Mission duration | Planned: 15 years[1] Final: 11 years, 4 months, 24 days[2] |
Spacecraft properties | |
Bus | DFH-4[3] |
Manufacturer | China Academy of Space Technology[4] |
Launch mass | 5,049 kg (11,131 lb)[3] |
Dimensions | 2.36 × 2.1 × 4 m (7.7 × 6.9 × 13.1 ft)[5] |
Power | 7.75 kW[4] |
Start of mission | |
Launch date | 29 October 2008, 16:53UTC[6] |
Rocket | Long March 3B/E[4] |
Launch site | Xichang, LC-2[3] |
Entered service | January 2009[1] |
End of mission | |
Disposal | Loss of spacecraft |
Declared | 25 March 2020[2] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 78° West[1] |
Semi-major axis | 42,448.3 km (26,376.2 mi) |
Eccentricity | 0.0056487 |
Perigee altitude | 35,830.4 km (22,264.0 mi) |
Apogee altitude | 36,309.9 km (22,561.9 mi) |
Inclination | 0.0472° |
Epoch | 24 March 2020, 05:04:06 UTC[7] |
Transponders | |
Band | 14 × C band 12 × Ku band 2 × Ka band[8] |
Coverage area | South America (C band) Venezuela region (Ku and Ka)[8] |
VeneSat-1, also known as Simón Bolívar (named after Venezuelan independence fighter Simón Bolívar), was the first Venezuelan satellite.[3] It was designed, built and launched by the CGWIC subsidiary of the China Aerospace Science and Technology Corporation.[3] It was a communications satellite operating from a geosynchronous orbit. The satellite was launched on a Chinese Long March 3B carrier rocket from Xichang Satellite Launch Center Launch Complex 2 on 29 October 2008 at 16:53 UTC.[9]