ORBCOMM FM 117, 41188
Orbit data source: Space-Track
ORBCOMM FM 117, 41188 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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41188 intel report (Beta)
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TLE from 1 day ago
0 ORBCOMM FM 117
1 41188U 15081K 25198.69622041 .00000492 00000-0 14220-3 0 9999
2 41188 47.0025 321.6407 0002497 118.1564 241.9574 14.58193338511298
TLE epoch observation values (Epoch: 2025-07-17T16:42:33.443Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 117 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 | 2025-07-18 17:55:01.756Z | 275.237° WNW | 2025-07-18 17:58:01.756Z | 211.117° SW | 32.487° | 2025-07-18 18:02:01.756Z | 151.929° SSE |
6 mins | 2025-07-19 10:00:01.756Z | 177.812° S | 2025-07-19 10:02:01.756Z | 142.719° SSE | 24.986° | 2025-07-19 10:06:01.756Z | 82.796° E |
8 mins | 2025-07-19 11:42:01.756Z | 250.807° W | 2025-07-19 11:45:01.756Z | 288.798° WNW | 43.032° | 2025-07-19 11:50:01.756Z | 59.771° ENE |
8 mins | 2025-07-19 13:26:01.756Z | 292.512° NW | 2025-07-19 13:29:01.756Z | 340.691° N | 30.855° | 2025-07-19 13:34:01.756Z | 61.732° ENE |
8 mins | 2025-07-19 15:10:01.756Z | 306.225° NW | 2025-07-19 15:14:01.756Z | 24.516° NE | 34.794° | 2025-07-19 15:18:01.756Z | 85.193° E |
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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