STTW-4
Satellite information STTW-4
| Spacetrack Directory Name | STTW-4 |
| Alternative name | SHIYAN TONGBU TONGXING WEIXING 4, DONG FANG HONG-2A 4, DFH-2A 4, CHINASAT 3, ZHONGXING 3, ZX 3 |
| Follow STTW-4 | STTW-4 Tracker |
| Pass predictions STTW-4 | Pass predictions STTW-4 |
| Orbit launches |
1990-02-04 (36 years ago)
|
| Days in orbit | 13377 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 35768 km |
| Apogee | 35816 km |
| Orbit slope (inclination) | 14.11° |
| Laps per day | 1 |
| Height STTW-4 | 35791.58 km |
Additional information STTW-4
STTW-4, 20473 is a payload satellite owned by Chinasat (CN) in GEO that was launched on Sun, 04 Feb 1990 UTC via a CHANG ZHENG 3 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 STTW-4 Date of exalting 04.02.1990y. Average height of ISS STTW-4 hundred 35791.58 km. Average velocity STTW-4 is 11068.32 km/h. Inclination STTW-4 satellite 14.12°.TLE
Average velocity STTW-4
Average inclination STTW-4
Mean right ascension of the ascending node (RAAN) STTW-4
Mean argument of perigee STTW-4
Mean semi-major axis of the orbit STTW-4
Mean orbital eccentricity STTW-4
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