GLOBALSTAR M101, 100330
Orbit data source: Space-Track
GLOBALSTAR M101, 100330 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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100330 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 M101
1 A0330U 26185F 26280.90857289 .00000044 00000-0 52439-4 0 9999
2 A0330 51.9995 10.8734 0008165 40.6885 319.4676 14.54207127 7736Epoch: 2026-10-07T21:48Z
TLE epoch observation values (Epoch: 2026-10-07T21:48:20.697Z)
Latitude
-0.00004°
Longitude
27.23512°
Altitude
708.291 km
Speed
7.505 km/s
True Right ascension
00h 43m 29s
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
01:31:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
718.16 km
Perigee altitude
706.582 km
Semi-major axis
7,090.508 km
Eccentricity
0.00082
Inclination
51.9995°
RAAN
10.8734°
Arg. of periapsis
40.6885°
True anomaly
319.40675°
Mean anomaly
319.4676°
Eccentric anomaly
319.43718°
Mean motion
3.63519 °/min
Orbital period
99.03 mins
BSTAR
0.000052439
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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 M101 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 06:43:16.491Z | 318.161° NNW | 2026-10-24 06:46:16.491Z | 0.632° NNE | 20.228° | 2026-10-24 06:49:16.491Z | 40.946° NE |
| 6 mins | 2026-10-24 08:28:16.491Z | 336.335° NNW | 2026-10-24 08:30:16.491Z | 10.073° NNE | 28.45° | 2026-10-24 08:34:16.491Z | 74.551° E |
| 8 mins | 2026-10-24 10:11:16.491Z | 306.482° NW | 2026-10-24 10:14:16.491Z | 281.55° WNW | 80.087° | 2026-10-24 10:19:16.491Z | 131.627° SE |
| 7 mins | 2026-10-25 02:19:16.491Z | 185.772° SSW | 2026-10-25 02:22:16.491Z | 129.118° SE | 35.308° | 2026-10-25 02:26:16.491Z | 69.424° E |
| 7 mins | 2026-10-25 04:02:16.491Z | 262.585° W | 2026-10-25 04:05:16.491Z | 325.141° NNW | 49.051° | 2026-10-25 04:09:16.491Z | 40.881° NE |
| 6 mins | 2026-10-25 05:47:16.491Z | 314.043° NW | 2026-10-25 05:49:16.491Z | 343.82° N | 21.759° | 2026-10-25 05:53:16.491Z | 39.037° 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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