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 via an FALCON 9 launch vehicle 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.
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100329 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
MDARM/RLABLB
Mission
Operational Commercial Communications
Bus & Motor
C-3, AOCS
Mass
850 kg wet, ~800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Cyl + 2 Pan, 4.5 m
Radar Cross Section
16.199 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 GLOBALSTAR M106
1 A0329U 26185E 26296.73480420 .00000270 00000-0 89034-4 0 9996
2 A0329 51.9967 302.6678 0010261 85.1353 275.0775 14.63443792 10052Epoch: 2026-10-23T17:38Z
TLE epoch observation values (Epoch: 2026-10-23T17:38:07.082Z)
Latitude
-0.00002°
Longitude
5.98718°
Altitude
682.194 km
Speed
7.517 km/s
True Right ascension
20h 10m 40s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:32:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.754 km
Perigee altitude
675.264 km
Semi-major axis
7,060.646 km
Eccentricity
0.00103
Inclination
51.9967°
RAAN
302.6678°
Arg. of periapsis
85.1353°
True anomaly
274.96037°
Mean anomaly
275.0775°
Eccentric anomaly
275.01893°
Mean motion
3.65828 °/min
Orbital period
98.41 mins
BSTAR
0.000089034
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Other satellites on launch #185 in the year 2026 (2026-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GLOBALSTAR M106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-24 07:07:07.764Z | 319.446° NNW | 2026-10-24 07:10:07.764Z | 359.111° N | 19.435° | 2026-10-24 07:13:07.764Z | 42.948° NE |
| 7 mins | 2026-10-24 08:51:07.764Z | 328.234° NNW | 2026-10-24 08:54:07.764Z | 23.555° NE | 35.623° | 2026-10-24 08:58:07.764Z | 89.454° E |
| 7 mins | 2026-10-24 10:34:07.764Z | 292.842° NW | 2026-10-24 10:37:07.764Z | 218.015° SW | 54.349° | 2026-10-24 10:41:07.764Z | 148.93° SSE |
| 7 mins | 2026-10-25 02:35:07.764Z | 202.453° SSW | 2026-10-25 02:38:07.764Z | 140.392° SSE | 49.169° | 2026-10-25 02:42:07.764Z | 64.123° ENE |
| 7 mins | 2026-10-25 04:18:07.764Z | 275.899° WNW | 2026-10-25 04:21:07.764Z | 337.186° NNW | 37.742° | 2026-10-25 04:25:07.764Z | 39.808° NE |
| 5 mins | 2026-10-25 06:03:07.764Z | 329.154° NNW | 2026-10-25 06:05:07.764Z | 1.279° NNE | 19.567° | 2026-10-25 06:08:07.764Z | 40.379° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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