ORBCOMM FM 118, 41183
Orbit data source: Space-Track
ORBCOMM FM 118, 41183 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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41183 intel report (Beta)
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TLE from 4 hours ago
0 ORBCOMM FM 118
1 41183U 15081E 25199.54381079 .00000418 00000-0 12621-3 0 9993
2 41183 47.0037 138.5255 0003718 297.7369 62.3139 14.58226919509107
TLE epoch observation values (Epoch: 2025-07-18T13:03:05.252Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 118 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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8 mins | 2025-07-18 23:07:07.396Z | 220.155° SW | 2025-07-18 23:10:07.396Z | 160.76° S | 40.868° | 2025-07-18 23:15:07.396Z | 66.994° ENE |
7 mins | 2025-07-19 00:51:07.396Z | 280.048° WNW | 2025-07-19 00:54:07.396Z | 347.968° N | 36.202° | 2025-07-19 00:58:07.396Z | 55.631° ENE |
7 mins | 2025-07-19 02:35:07.396Z | 306.237° NW | 2025-07-19 02:38:07.396Z | 0.281° NNE | 30.96° | 2025-07-19 02:42:07.396Z | 67.976° E |
8 mins | 2025-07-19 04:19:07.396Z | 304.604° NW | 2025-07-19 04:22:07.396Z | 5.341° NNE | 42.756° | 2025-07-19 04:27:07.396Z | 107.66° ESE |
6 mins | 2025-07-19 06:03:07.396Z | 267.793° W | 2025-07-19 06:05:07.396Z | 233.045° WSW | 27.335° | 2025-07-19 06:09:07.396Z | 164.87° 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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