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, 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 M100
1 A0332U 26185H 26296.72855625 .00000272 00000-0 89178-4 0 9993
2 A0332 51.9964 302.6278 0009575 84.6201 275.5847 14.63485613 10054Epoch: 2026-10-23T17:29Z
TLE epoch observation values (Epoch: 2026-10-23T17:29:07.259Z)
Latitude
-0.00005°
Longitude
8.20258°
Altitude
682.042 km
Speed
7.517 km/s
True Right ascension
20h 10m 30s
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
01:30:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.135 km
Perigee altitude
675.614 km
Semi-major axis
7,060.511 km
Eccentricity
0.00096
Inclination
51.9964°
RAAN
302.6278°
Arg. of periapsis
84.6201°
True anomaly
275.47549°
Mean anomaly
275.5847°
Eccentric anomaly
275.53009°
Mean motion
3.65838 °/min
Orbital period
98.4 mins
BSTAR
0.000089178
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-24 06:58:15.227Z | 324.146° NNW | 2026-10-24 07:01:15.227Z | 7.957° NNE | 19.194° | 2026-10-24 07:04:15.227Z | 47.128° ENE |
| 6 mins | 2026-10-24 08:42:15.227Z | 335.244° NNW | 2026-10-24 08:44:15.227Z | 11.697° NNE | 31.945° | 2026-10-24 08:48:15.227Z | 82.494° E |
| 8 mins | 2026-10-24 10:24:15.227Z | 299.28° NW | 2026-10-24 10:27:15.227Z | 249.293° W | 61.056° | 2026-10-24 10:32:15.227Z | 142.115° SSE |
| 7 mins | 2026-10-25 02:26:15.227Z | 191.408° SSW | 2026-10-25 02:29:15.227Z | 120.195° SE | 41.08° | 2026-10-25 02:33:15.227Z | 64.605° ENE |
| 7 mins | 2026-10-25 04:08:15.227Z | 267.771° W | 2026-10-25 04:11:15.227Z | 322.898° NNW | 41.521° | 2026-10-25 04:15:15.227Z | 38.552° NE |
| 5 mins | 2026-10-25 05:53:15.227Z | 322.555° NNW | 2026-10-25 05:55:15.227Z | 354.093° N | 20.22° | 2026-10-25 05:58:15.227Z | 35.97° 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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