GEESAT 2-01
Satellite information GEESAT 2-01 - 2024-023A
| Spacetrack Directory Name | GEESAT 2-01 |
| Alternative name | 2024-023A |
| Follow GEESAT 2-01 | GEESAT 2-01 Tracker |
| Pass predictions GEESAT 2-01 | Pass predictions GEESAT 2-01 |
| Orbit launches |
2024-02-02 (2 years ago)
|
| Days in orbit | 979 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 595 km |
| Apogee | 606 km |
| Orbit slope (inclination) | 49.99° |
| Laps per day | 15 |
| Height GEESAT 2-01 | 623.11 km |
Additional information GEESAT 2-01
GEESAT 2-01, 58905 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 02 Feb 2024 UTC via a CHANG ZHENG 2C 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 GEESAT 2-01 Date of exalting 02.02.2024y. Average height of ISS GEESAT 2-01 hundred 623.11 km. Average velocity GEESAT 2-01 is 27177.81 km/h. Inclination GEESAT 2-01 satellite 49.99°.TLE
Average velocity GEESAT 2-01
Average inclination GEESAT 2-01
Mean right ascension of the ascending node (RAAN) GEESAT 2-01
Mean argument of perigee GEESAT 2-01
Mean semi-major axis of the orbit GEESAT 2-01
Mean orbital eccentricity GEESAT 2-01
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