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: 2 days ago
TLE from 2 days ago
0 ORBCOMM FM 108
1 41187U 15081J 25287.25043436 .00001154 00000-0 28300-3 0 9994
2 41187 47.0048 264.6046 0001638 159.6453 200.4498 14.58392466524179
TLE epoch observation values (Epoch: 2025-10-14T06:00:37.528Z)
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 | 2025-10-16 00:55:48.244Z | 214.751° SW | 2025-10-16 00:59:48.244Z | 156.241° SSE | 36.054° | 2025-10-16 01:04:48.244Z | 70.416° E |
8 mins | 2025-10-16 02:39:48.244Z | 266.984° W | 2025-10-16 02:43:48.244Z | 348.614° N | 38.649° | 2025-10-16 02:47:48.244Z | 56.105° ENE |
7 mins | 2025-10-16 04:24:48.244Z | 304.511° NW | 2025-10-16 04:27:48.244Z | 0.552° NNE | 30.521° | 2025-10-16 04:31:48.244Z | 64.877° ENE |
8 mins | 2025-10-16 06:08:48.244Z | 307.696° NW | 2025-10-16 06:11:48.244Z | 12.247° NNE | 40.277° | 2025-10-16 06:16:48.244Z | 100.683° ESE |
8 mins | 2025-10-16 07:51:48.244Z | 282.058° WNW | 2025-10-16 07:55:48.244Z | 204.778° SW | 32.676° | 2025-10-16 07:59:48.244Z | 150.209° 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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