GLOBALSTAR M080

NORAD 38041· COSPAR 2011-080B· Active satellite· Communications· LEO

Launch

Launched on Dec 28, 2011 from 31/6, Kazakhstan aboard a Soyuz 2.1a Fregat-M.

Soyuz-2.1a/Fregat | 6 x Globalstar-2 →

Live · TLE epoch 2026-09-09 02:51 UTC

Orbit class

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

Operator

Globalstar

Country

Globalstar

Manufacturer

Thales Alenia Space

Launched

Dec 28, 2011

Mass

—

Apogee

1,422 km

Perigee

1,420 km

Inclination

52.00°

Period

1.90 h

Altitude history

Apogee and perigee for GLOBALSTAR M080 across 103 days of archived orbital elements (104 element sets, one per day).

Trend

Stable

Change

+0.0 km

Rate

+0.00 km/day

Now

1420 × 1422 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

5 other catalogued objects still in orbit from launch 2011-080 (Soyuz-2.1a/Fregat | 6 x Globalstar-2).

Sources & further reading

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