ORBCOMM FM 105, 41181
Orbit data source: Space-Track
ORBCOMM FM 105, 41181 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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41181 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ORBCOMM FM 105
1 41181U 15081C 25257.40267922 .00000139 00000-0 83801-4 0 9990
2 41181 47.0010 148.4040 0002040 344.6273 15.4545 14.45286750513651
TLE epoch observation values (Epoch: 2025-09-14T09:39:51.484Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 105 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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8 mins | 2025-09-15 19:00:40.215Z | 203.978° SW | 2025-09-15 19:04:40.215Z | 142.565° SSE | 31.746° | 2025-09-15 19:08:40.215Z | 77.825° E |
8 mins | 2025-09-15 20:45:40.215Z | 261.259° W | 2025-09-15 20:48:40.215Z | 312.061° NW | 41.038° | 2025-09-15 20:53:40.215Z | 58.123° ENE |
8 mins | 2025-09-15 22:30:40.215Z | 297.313° NW | 2025-09-15 22:34:40.215Z | 10.96° NNE | 31.074° | 2025-09-15 22:38:40.215Z | 64.423° ENE |
8 mins | 2025-09-16 00:15:40.215Z | 306.19° NW | 2025-09-16 00:19:40.215Z | 31.034° NE | 38.38° | 2025-09-16 00:23:40.215Z | 92.922° ESE |
8 mins | 2025-09-16 02:00:40.215Z | 283.819° WNW | 2025-09-16 02:03:40.215Z | 226.625° WSW | 37.878° | 2025-09-16 02:08:40.215Z | 142.156° 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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