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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TLE from 9 hours ago
0 ORBCOMM FM 116
1 41189U 15081L 25199.57463086 .00000790 00000-0 20571-3 0 9997
2 41189 47.0027 47.3292 0002217 298.9225 61.1438 14.58266792510235
TLE epoch observation values (Epoch: 2025-07-18T13:47:28.106Z)
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
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 00:12:01.028Z | 276.371° WNW | 2025-07-19 00:16:01.028Z | 214.859° SW | 24.943° | 2025-07-19 00:19:01.028Z | 170.595° S |
7 mins | 2025-07-19 16:17:01.028Z | 200.47° SSW | 2025-07-19 16:20:01.028Z | 143.205° SSE | 32.633° | 2025-07-19 16:24:01.028Z | 76.228° E |
8 mins | 2025-07-19 18:00:01.028Z | 263.157° W | 2025-07-19 18:03:01.028Z | 312.026° NW | 39.748° | 2025-07-19 18:08:01.028Z | 57.824° ENE |
7 mins | 2025-07-19 19:45:01.028Z | 306.115° NW | 2025-07-19 19:48:01.028Z | 9.262° NNE | 30.266° | 2025-07-19 19:52:01.028Z | 64.8° ENE |
8 mins | 2025-07-19 21:28:01.028Z | 305.445° NW | 2025-07-19 21:32:01.028Z | 27.725° NE | 38.375° | 2025-07-19 21:36:01.028Z | 93.76° ESE |
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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