GEESAT-2 06

NORAD 58910· COSPAR 2024-023F· Active satellite· Other / Unclassified· LEO

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 2026-10-23 19:34 UTC

Orbit class

LEO — Low Earth Orbit (circular, < 2,000 km)

Operator

Chinese Government

Country

China

Manufacturer

—

Launched

Feb 2, 2024

Mass

—

Apogee

563 km

Perigee

555 km

Inclination

49.99°

Period

1.59 h

Altitude history

Apogee and perigee for GEESAT-2 06 across 59 days of archived orbital elements (60 element sets, one per day).

Trend

Decaying

Change

-1.4 km

Rate

-0.02 km/day

Now

555 × 563 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 07 · 58911
GEESAT-2 08 · 58912
GEESAT-2 09 · 58913
GEESAT-2 10 · 58914
GEESAT-2 11 · 58915

Sources & further reading

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