GEESAT-2 10
Launch
Launched on Feb 2, 2024 from Launch Complex 3 (LC-3/LA-1), China aboard a Long March 2C.
Long March 2C | Geely Constellation Group 02 →Live · TLE epoch 2026-09-08 14:25 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
Chinese Government
Country
China
Manufacturer
—
Launched
Feb 2, 2024
Mass
—
Apogee
633 km
Perigee
619 km
Inclination
50.00°
Period
1.62 h
Altitude history
Apogee and perigee for GEESAT-2 10 across 14 days of archived orbital elements (15 element sets, one per day).
Trend
Stable
Change
-0.1 km
Rate
-0.01 km/day
Now
619 × 633 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
Launched with
10 other catalogued objects still in orbit from launch 2024-023 (Long March 2C | Geely Constellation Group 02).
- GEESAT-2 01 · 58905
- GEESAT-2 02 · 58906
- GEESAT-2 03 · 58907
- GEESAT-2 04 · 58908
- GEESAT-2 05 · 58909
- GEESAT-2 06 · 58910
- GEESAT-2 07 · 58911
- GEESAT-2 08 · 58912
- GEESAT-2 09 · 58913
- GEESAT-2 11 · 58915
Sources & further reading
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