GEESAT 3-08
Satellite information GEESAT 3-08 - 2024-159H
| Spacetrack Directory Name | GEESAT 3-08 |
| Alternative name | 2024-159H |
| Follow GEESAT 3-08 | GEESAT 3-08 Tracker |
| Pass predictions GEESAT 3-08 | Pass predictions GEESAT 3-08 |
| Orbit launches |
2024-09-05 (2 years ago)
|
| Days in orbit | 772 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 553 km |
| Apogee | 565 km |
| Orbit slope (inclination) | 50.01° |
| Laps per day | 15 |
| Height GEESAT 3-08 | 620.86 km |
Additional information GEESAT 3-08
GEESAT 3-08, 61018 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 05 Sep 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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 GEESAT 3-08 Date of exalting 05.09.2024y. Average height of ISS GEESAT 3-08 hundred 620.86 km. Average velocity GEESAT 3-08 is 27182.16 km/h. Inclination GEESAT 3-08 satellite 50°.TLE
Average velocity GEESAT 3-08
Average inclination GEESAT 3-08
Mean right ascension of the ascending node (RAAN) GEESAT 3-08
Mean argument of perigee GEESAT 3-08
Mean semi-major axis of the orbit GEESAT 3-08
Mean orbital eccentricity GEESAT 3-08
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