Showing default

GLOBALSTAR M106, 100329

Orbit data source: Space-Track

GLOBALSTAR M106, 100329 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sun, 16 Aug 2026 UTC launched from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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.

Loading next visibility...
Identifier
100329, 2026-185E
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MDARM/RLABLB
Mission
Operational spacecraft
Bus & Motor
C-3, AOCS
Mass
850 kg wet, ~800 kg dry
Launch date (UTC)
2026-08-16 (3 weeks ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
TRAP CYL + 2 PAN, 7.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 GLOBALSTAR M106
1 A0329U 26185E   26251.12055692  .00000245  00000-0  83365-4 0  9992
2 A0329  51.9960 138.8006 0009047 307.3386  52.6746 14.63872509  3370
Epoch: 2026-09-08T02:53Z
TLE epoch observation values (Epoch: 2026-09-08T02:53:36.117Z)
Latitude
-0.00003°
Longitude
108.20856°
Altitude
677.581 km
Speed
7.521 km/s
True Right ascension
09h 15m 12s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:34:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
687.517 km
Perigee altitude
674.744 km
Semi-major axis
7,059.267 km
Eccentricity
0.0009
Inclination
51.996°
RAAN
138.8006°
Arg. of periapsis
307.3386°
True anomaly
52.7571°
Mean anomaly
52.6746°
Eccentric anomaly
52.71584°
Mean motion
3.65935 °/min
Orbital period
98.38 mins
BSTAR
0.000083365
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|