ORBCOMM FM 116, 41189
Orbit data source: Space-Track
ORBCOMM FM 116, 41189 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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41189 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 116
1 41189U 15081L 25257.39905490 .00000599 00000-0 16446-3 0 9995
2 41189 47.0017 134.1664 0001876 227.1975 132.8753 14.58377756518673
TLE epoch observation values (Epoch: 2025-09-14T09:34:38.343Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 116 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 18:39:48.983Z | 220.005° SW | 2025-09-15 18:42:48.983Z | 158.051° S | 40.969° | 2025-09-15 18:47:48.983Z | 66.889° ENE |
7 mins | 2025-09-15 20:23:48.983Z | 280.543° WNW | 2025-09-15 20:26:48.983Z | 350.198° N | 36.131° | 2025-09-15 20:30:48.983Z | 55.91° ENE |
7 mins | 2025-09-15 22:07:48.983Z | 306.836° NW | 2025-09-15 22:10:48.983Z | 2.274° NNE | 30.962° | 2025-09-15 22:14:48.983Z | 68.458° E |
8 mins | 2025-09-15 23:51:48.983Z | 304.883° NW | 2025-09-15 23:54:48.983Z | 12.405° NNE | 42.893° | 2025-09-15 23:59:48.983Z | 107.84° ESE |
6 mins | 2025-09-16 01:35:48.983Z | 266.642° W | 2025-09-16 01:37:48.983Z | 230.734° WSW | 27.411° | 2025-09-16 01:41:48.983Z | 164.137° 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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