GEESAT 2-04
Satellite information GEESAT 2-04 - 2024-023D
| Spacetrack Directory Name | GEESAT 2-04 |
| Alternative name | 2024-023D |
| Follow GEESAT 2-04 | GEESAT 2-04 Tracker |
| Pass predictions GEESAT 2-04 | Pass predictions GEESAT 2-04 |
| Orbit launches |
2024-02-02 (2 years ago)
|
| Days in orbit | 942 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 594 km |
| Apogee | 606 km |
| Orbit slope (inclination) | 49.99° |
| Laps per day | 15 |
| Height GEESAT 2-04 | 583.58 km |
Additional information GEESAT 2-04
GEESAT 2-04, 58908 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 2-04 Date of exalting 02.02.2024y. Average height of ISS GEESAT 2-04 hundred 583.58 km. Average velocity GEESAT 2-04 is 27254.94 km/h. Inclination GEESAT 2-04 satellite 49.99°.TLE
Average velocity GEESAT 2-04
Average inclination GEESAT 2-04
Mean right ascension of the ascending node (RAAN) GEESAT 2-04
Mean argument of perigee GEESAT 2-04
Mean semi-major axis of the orbit GEESAT 2-04
Mean orbital eccentricity GEESAT 2-04
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