VENESAT-1
Satellite information VENESAT-1 - SIMON BOLIVAR
| Spacetrack Directory Name | VENESAT-1 |
| Alternative name | SIMON BOLIVAR |
| Follow VENESAT-1 | VENESAT-1 Tracker |
| Pass predictions VENESAT-1 | Pass predictions VENESAT-1 |
| Orbit launches |
2008-10-29 (17 years ago)
|
| Days in orbit | 6515 |
| Country/organisation of origin | Wenezuela (VENZ) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Categories | |
| Perigee | 35815 km |
| Apogee | 36323 km |
| Orbit slope (inclination) | 5.94° |
| Laps per day | 1 |
| Orbit | GEO |
| Height VENESAT-1 | 36069.92 km |
Additional information VENESAT-1
Venesat-1, also known as Simón Bolívar, is the first Venezuelan satellite. It was designed, built, launched, controlled and monitored by the CGWIC subsidiary of the China Aerospace Science and Technology Corporation. It is a communications satellite, which will be operated from a geosynchronous orbit. It was launched on a Chinese Long March 3B carrier rocket, from LA-2 at the Xichang Satellite Launch Centre, at 16:53 UTC on 29 October 2008.Venesat-1 will be operated by Venezuela's Ministry of Science and Technology. It carries 12 G-band (IEEE's C band) and 14 J-band (IEEE Ku band) transponders. It has a mass of 5,100 kilograms (11,200 lb), and an expected service life of 15 years. It is based on the DFH-4 satellite bus. The satellite occupies an orbital slot, 78-West, designated for Uruguay and ceded to Venezuela by mutual accord.
satellite VENESAT-1 Date of exalting 29.10.2008y. Average height of ISS VENESAT-1 hundred 36069.92 km. Average velocity VENESAT-1 is 11032.02 km/h. Inclination VENESAT-1 satellite 5.92°.TLE
Average velocity VENESAT-1
Average inclination VENESAT-1
Mean right ascension of the ascending node (RAAN) VENESAT-1
Mean argument of perigee VENESAT-1
Mean semi-major axis of the orbit VENESAT-1
Mean orbital eccentricity VENESAT-1
ISS
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