GLOBALSTAR M102, 100326
Orbit data source: Space-Track
GLOBALSTAR M102, 100326 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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100326 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 M102
1 A0326U 26185B 26296.74090286 .00000273 00000-0 89668-4 0 9997
2 A0326 51.9968 302.7032 0010622 86.7375 273.4797 14.63335346 10058Epoch: 2026-10-23T17:46Z
TLE epoch observation values (Epoch: 2026-10-23T17:46:54.007Z)
Latitude
0.00004°
Longitude
3.8211°
Altitude
682.729 km
Speed
7.517 km/s
True Right ascension
20h 10m 48s
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
01:29:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
690.358 km
Perigee altitude
675.357 km
Semi-major axis
7,060.994 km
Eccentricity
0.00106
Inclination
51.9968°
RAAN
302.7032°
Arg. of periapsis
86.7375°
True anomaly
273.3582°
Mean anomaly
273.4797°
Eccentric anomaly
273.41895°
Mean motion
3.65801 °/min
Orbital period
98.41 mins
BSTAR
0.000089668
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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 M102 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 07:16:44.302Z | 323.589° NNW | 2026-10-24 07:19:44.302Z | 5.567° NNE | 19.904° | 2026-10-24 07:22:44.302Z | 48.049° ENE |
| 7 mins | 2026-10-24 09:00:44.302Z | 330.099° NNW | 2026-10-24 09:03:44.302Z | 35.288° NE | 38.879° | 2026-10-24 09:07:44.302Z | 95.464° ESE |
| 8 mins | 2026-10-24 10:42:44.302Z | 292.703° NW | 2026-10-24 10:45:44.302Z | 243.639° WSW | 44.922° | 2026-10-24 10:50:44.302Z | 152.851° SSE |
| 7 mins | 2026-10-25 02:44:44.302Z | 207.29° SW | 2026-10-25 02:47:44.302Z | 124.078° SE | 57.097° | 2026-10-25 02:51:44.302Z | 60.098° ENE |
| 7 mins | 2026-10-25 04:27:44.302Z | 282.877° WNW | 2026-10-25 04:30:44.302Z | 344.756° N | 34.029° | 2026-10-25 04:34:44.302Z | 40.552° NE |
| 5 mins | 2026-10-25 06:11:44.302Z | 320.722° NNW | 2026-10-25 06:13:44.302Z | 349.224° N | 19.227° | 2026-10-25 06:16:44.302Z | 33.699° 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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