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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TLE from 16 hours ago
0 ORBCOMM FM 108
1 41187U 15081J 25199.68925804 .00000553 00000-0 15517-3 0 9999
2 41187 47.0062 318.1991 0001834 115.0757 245.0319 14.58190842511391
TLE epoch observation values (Epoch: 2025-07-18T16:32:31.894Z)
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
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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7 mins | 2025-07-19 10:49:40.467Z | 214.651° SW | 2025-07-19 10:52:40.467Z | 151.636° SSE | 39.066° | 2025-07-19 10:56:40.467Z | 71.237° E |
8 mins | 2025-07-19 12:32:40.467Z | 271.384° WNW | 2025-07-19 12:36:40.467Z | 353.704° N | 37.057° | 2025-07-19 12:40:40.467Z | 56.332° ENE |
7 mins | 2025-07-19 14:17:40.467Z | 306.697° NW | 2025-07-19 14:20:40.467Z | 4.021° NNE | 30.672° | 2025-07-19 14:24:40.467Z | 67.31° ENE |
7 mins | 2025-07-19 16:01:40.467Z | 306.667° NW | 2025-07-19 16:04:40.467Z | 18° NNE | 41.826° | 2025-07-19 16:08:40.467Z | 102.206° ESE |
7 mins | 2025-07-19 17:44:40.467Z | 278.494° WNW | 2025-07-19 17:47:40.467Z | 231.204° WSW | 29.767° | 2025-07-19 17:51:40.467Z | 160.033° 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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