ORBCOMM FM 108, 41187
Orbit data source: Space-Track
ORBCOMM FM 108, 41187 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Tue, 22 Dec 2015 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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41187 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ORBCOMM FM 108
1 41187U 15081J 25258.40738048 .00000792 00000-0 20615-3 0 9997
2 41187 47.0058 40.8584 0002031 353.9870 6.0991 14.58302194519969
TLE epoch observation values (Epoch: 2025-09-15T09:46:37.673Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 108 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. |
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9 mins | 2025-09-16 12:15:23.977Z | 218.259° SW | 2025-09-16 12:20:23.977Z | 123.738° SE | 37.211° | 2025-09-16 12:24:23.977Z | 70.028° E |
7 mins | 2025-09-16 14:00:23.977Z | 273.429° WNW | 2025-09-16 14:03:23.977Z | 337.63° N | 37.882° | 2025-09-16 14:07:23.977Z | 54.853° ENE |
7 mins | 2025-09-16 15:44:23.977Z | 303.069° NW | 2025-09-16 15:47:23.977Z | 353.844° N | 30.411° | 2025-09-16 15:51:23.977Z | 64.197° ENE |
8 mins | 2025-09-16 17:28:23.977Z | 305.724° NW | 2025-09-16 17:31:23.977Z | 356.757° N | 40.491° | 2025-09-16 17:36:23.977Z | 102.186° ESE |
7 mins | 2025-09-16 19:12:23.977Z | 274.417° WNW | 2025-09-16 19:15:23.977Z | 213.284° SW | 31.409° | 2025-09-16 19:19:23.977Z | 154.076° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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