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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TLE from 15 hours ago
0 ORBCOMM FM 105
1 41181U 15081C 25199.88486163 .00000101 00000-0 73192-4 0 9998
2 41181 47.0021 54.4823 0001280 103.7528 256.3495 14.45238609505336
TLE epoch observation values (Epoch: 2025-07-18T21:14:12.044Z)
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
Observer location: undefined°, undefined°
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 | 2025-07-19 17:21:06.368Z | 220.123° SW | 2025-07-19 17:24:06.368Z | 156.899° SSE | 41.47° | 2025-07-19 17:29:06.368Z | 66.827° ENE |
8 mins | 2025-07-19 19:05:06.368Z | 274.765° WNW | 2025-07-19 19:09:06.368Z | 351.34° N | 36.572° | 2025-07-19 19:13:06.368Z | 55.881° ENE |
7 mins | 2025-07-19 20:51:06.368Z | 307.645° NW | 2025-07-19 20:54:06.368Z | 3.463° NNE | 31.95° | 2025-07-19 20:58:06.368Z | 69.012° E |
9 mins | 2025-07-19 22:35:06.368Z | 301.725° NW | 2025-07-19 22:39:06.368Z | 16.137° NNE | 43.533° | 2025-07-19 22:44:06.368Z | 109.331° ESE |
7 mins | 2025-07-20 00:20:06.368Z | 274.289° WNW | 2025-07-20 00:23:06.368Z | 228.496° WSW | 27.219° | 2025-07-20 00:27:06.368Z | 165.955° S |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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