GLOBALSTAR M104, 100328
Orbit data source: Space-Track
GLOBALSTAR M104, 100328 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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100328 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: 2 weeks ago
TLE from 2 weeks ago
0 GLOBALSTAR M104
1 A0328U 26185D 26281.70981294 -.00000099 00000-0 36996-4 0 9990
2 A0328 51.9957 15.2779 0011419 35.1199 325.0478 13.95580413 598Epoch: 2026-10-08T17:02Z
TLE epoch observation values (Epoch: 2026-10-08T17:02:07.838Z)
Latitude
-0.00003°
Longitude
102.40347°
Altitude
903.051 km
Speed
7.405 km/s
True Right ascension
01h 01m 06s
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
01:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
917.881 km
Perigee altitude
901.237 km
Semi-major axis
7,287.696 km
Eccentricity
0.00114
Inclination
51.9957°
RAAN
15.2779°
Arg. of periapsis
35.1199°
True anomaly
324.97275°
Mean anomaly
325.0478°
Eccentric anomaly
325.01028°
Mean motion
3.48865 °/min
Orbital period
103.19 mins
BSTAR
0.000036996
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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 M104 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-24 06:21:17.881Z | 345.83° N | 2026-10-24 06:21:17.881Z | 345.83° N | 33.721° | 2026-10-24 06:26:17.881Z | 44.243° NE |
| 8 mins | 2026-10-24 08:07:17.881Z | 323.193° NNW | 2026-10-24 08:10:17.881Z | 3.195° NNE | 26.087° | 2026-10-24 08:15:17.881Z | 59.717° ENE |
| 9 mins | 2026-10-24 09:55:17.881Z | 321.261° NNW | 2026-10-24 09:59:17.881Z | 22.497° NNE | 45.498° | 2026-10-24 10:04:17.881Z | 95.905° ESE |
| 9 mins | 2026-10-24 11:43:17.881Z | 294.376° NW | 2026-10-24 11:47:17.881Z | 229.176° WSW | 52.562° | 2026-10-24 11:52:17.881Z | 153.543° SSE |
| 8 mins | 2026-10-25 02:46:17.881Z | 175.817° S | 2026-10-25 02:50:17.881Z | 123.633° SE | 27.584° | 2026-10-25 02:54:17.881Z | 76.351° E |
| 10 mins | 2026-10-25 04:33:17.881Z | 243.864° WSW | 2026-10-25 04:37:17.881Z | 311.225° NW | 70.769° | 2026-10-25 04:43:17.881Z | 49.263° ENE |
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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