SINOSAT 2
Satellite information SINOSAT 2 - SINOSAT 2 (XINNUO 2)
| Spacetrack Directory Name | SINOSAT 2 |
| Alternative name | SINOSAT 2 (XINNUO 2) |
| Follow SINOSAT 2 | SINOSAT 2 Tracker |
| Pass predictions SINOSAT 2 | Pass predictions SINOSAT 2 |
| Orbit launches |
2006-10-28 (19 years ago)
|
| Days in orbit | 7248 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 37827 km |
| Apogee | 38162 km |
| Orbit slope (inclination) | 14.61° |
| Laps per day | 1 |
| Height SINOSAT 2 | 37993.86 km |
Additional information SINOSAT 2
SINOSAT 2, 29516 is a payload satellite owned by Sinosat (CN) in GEO that was launched on Sat, 28 Oct 2006 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite SINOSAT 2 Date of exalting 28.10.2006y. Average height of ISS SINOSAT 2 hundred 37993.86 km. Average velocity SINOSAT 2 is 10790.27 km/h. Inclination SINOSAT 2 satellite 14.58°.TLE
Average velocity SINOSAT 2
Average inclination SINOSAT 2
Mean right ascension of the ascending node (RAAN) SINOSAT 2
Mean argument of perigee SINOSAT 2
Mean semi-major axis of the orbit SINOSAT 2
Mean orbital eccentricity SINOSAT 2
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