GLOBALSTAR M105, 100331
Orbit data source: Space-Track
GLOBALSTAR M105, 100331 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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100331 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: 19 hours ago
TLE from 19 hours ago
0 GLOBALSTAR M105
1 A0331U 26185G 26296.45799211 .00000275 00000-0 89861-4 0 9992
2 A0331 51.9960 303.8130 0009646 84.3479 275.8578 14.63502982 10011Epoch: 2026-10-23T10:59Z
TLE epoch observation values (Epoch: 2026-10-23T10:59:30.518Z)
Latitude
0.00005°
Longitude
107.05763°
Altitude
681.949 km
Speed
7.517 km/s
True Right ascension
20h 15m 15s
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
01:26:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.129 km
Perigee altitude
675.508 km
Semi-major axis
7,060.455 km
Eccentricity
0.00096
Inclination
51.996°
RAAN
303.813°
Arg. of periapsis
84.3479°
True anomaly
275.74783°
Mean anomaly
275.8578°
Eccentric anomaly
275.80282°
Mean motion
3.65842 °/min
Orbital period
98.4 mins
BSTAR
0.000089861
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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 M105 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 07:01:36.850Z | 319.154° NNW | 2026-10-24 07:04:36.850Z | 359.279° N | 19.344° | 2026-10-24 07:07:36.850Z | 42.471° NE |
| 7 mins | 2026-10-24 08:45:36.850Z | 329.168° NNW | 2026-10-24 08:48:36.850Z | 23.917° NE | 33.822° | 2026-10-24 08:52:36.850Z | 87.36° E |
| 7 mins | 2026-10-24 10:28:36.850Z | 295.414° NW | 2026-10-24 10:31:36.850Z | 216.236° SW | 59.627° | 2026-10-24 10:35:36.850Z | 145.598° SSE |
| 7 mins | 2026-10-25 02:29:36.850Z | 198.338° SSW | 2026-10-25 02:32:36.850Z | 137.655° SSE | 44.801° | 2026-10-25 02:36:36.850Z | 65.704° ENE |
| 7 mins | 2026-10-25 04:12:36.850Z | 273.885° WNW | 2026-10-25 04:15:36.850Z | 339.481° N | 39.864° | 2026-10-25 04:19:36.850Z | 40.773° NE |
| 6 mins | 2026-10-25 05:56:36.850Z | 316.756° NNW | 2026-10-25 05:58:36.850Z | 345.525° N | 19.763° | 2026-10-25 06:02:36.850Z | 40.65° 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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