ORBCOMM FM 114, 41179
Orbit data source: Space-Track
ORBCOMM FM 114, 41179 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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41179 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ORBCOMM FM 114
1 41179U 15081A 25257.34543043 .00000458 00000-0 13442-3 0 9998
2 41179 47.0018 225.7054 0001963 9.3659 350.7263 14.58333406517488
TLE epoch observation values (Epoch: 2025-09-14T08:17:25.189Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 114 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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7 mins | 2025-09-15 23:55:29.943Z | 192.513° SSW | 2025-09-15 23:58:29.943Z | 141.875° SSE | 27.978° | 2025-09-16 00:02:29.943Z | 79.869° E |
8 mins | 2025-09-16 01:38:29.943Z | 256.152° W | 2025-09-16 01:41:29.943Z | 304.843° NW | 42.101° | 2025-09-16 01:46:29.943Z | 58.962° ENE |
8 mins | 2025-09-16 03:22:29.943Z | 295.03° NW | 2025-09-16 03:25:29.943Z | 342.984° N | 30.442° | 2025-09-16 03:30:29.943Z | 63.167° ENE |
8 mins | 2025-09-16 05:06:29.943Z | 306.475° NW | 2025-09-16 05:10:29.943Z | 28.483° NE | 36.013° | 2025-09-16 05:14:29.943Z | 88.736° E |
8 mins | 2025-09-16 06:50:29.943Z | 288.468° WNW | 2025-09-16 06:53:29.943Z | 233.924° WSW | 40.414° | 2025-09-16 06:58:29.943Z | 135.83° SSE |
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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