GLOBALSTAR M100, 100332
Orbit data source: Space-Track
GLOBALSTAR M100, 100332 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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100332 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, 1.4 m
Radar Cross Section
16.199 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GLOBALSTAR M100
1 A0332U 26185H 26287.16798266 .00000353 00000-0 10466-3 0 9991
2 A0332 51.9976 343.7295 0009473 57.4607 302.7263 14.63476566 8652Epoch: 2026-10-14T04:01Z
TLE epoch observation values (Epoch: 2026-10-14T04:01:53.701Z)
Latitude
-0.00007°
Longitude
-99.46589°
Altitude
679.111 km
Speed
7.52 km/s
True Right ascension
22h 54m 55s
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
14:44:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.092 km
Perigee altitude
675.715 km
Semi-major axis
7,060.54 km
Eccentricity
0.00095
Inclination
51.9976°
RAAN
343.7295°
Arg. of periapsis
57.4607°
True anomaly
302.63492°
Mean anomaly
302.7263°
Eccentric anomaly
302.68062°
Mean motion
3.65836 °/min
Orbital period
98.4 mins
BSTAR
0.00010466
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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 M100 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-15 06:25:43.305Z | 221.637° SW | 2026-10-15 06:29:43.305Z | 116.056° SE | 72.028° | 2026-10-15 06:33:43.305Z | 55.938° ENE |
| 7 mins | 2026-10-15 08:09:43.305Z | 287.752° WNW | 2026-10-15 08:12:43.305Z | 342.573° N | 30.153° | 2026-10-15 08:16:43.305Z | 39.283° NE |
| 5 mins | 2026-10-15 09:54:43.305Z | 333.639° NNW | 2026-10-15 09:56:43.305Z | 5.038° NNE | 19.152° | 2026-10-15 09:59:43.305Z | 44.271° NE |
| 6 mins | 2026-10-15 11:37:43.305Z | 334.848° NNW | 2026-10-15 11:40:43.305Z | 31.543° NE | 29.016° | 2026-10-15 11:43:43.305Z | 76.693° E |
| 8 mins | 2026-10-15 13:19:43.305Z | 304.366° NW | 2026-10-15 13:23:43.305Z | 171.615° S | 71.386° | 2026-10-15 13:27:43.305Z | 135.448° SSE |
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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