ORBCOMM FM 115, 41186
Orbit data source: Space-Track
ORBCOMM FM 115, 41186 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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41186 intel report (Beta)
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TLE from 11 hours ago
0 ORBCOMM FM 115
1 41186U 15081H 25199.20173216 .00000322 00000-0 97305-4 0 9998
2 41186 46.9976 252.0484 0001597 240.2624 119.8104 14.62539691512312
TLE epoch observation values (Epoch: 2025-07-18T04:50:29.658Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2015 (2015-12-22 UTC)
ORBCOMM FM 115 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 | 2025-07-19 05:35:16.531Z | 194.434° SSW | 2025-07-19 05:39:16.531Z | 135.489° SSE | 25.22° | 2025-07-19 05:43:16.531Z | 80.076° E |
8 mins | 2025-07-19 07:18:16.531Z | 250.748° W | 2025-07-19 07:22:16.531Z | 358.786° N | 43.6° | 2025-07-19 07:26:16.531Z | 59.109° ENE |
8 mins | 2025-07-19 09:02:16.531Z | 292.45° WNW | 2025-07-19 09:05:16.531Z | 339.914° N | 30.465° | 2025-07-19 09:10:16.531Z | 61.768° ENE |
8 mins | 2025-07-19 10:46:16.531Z | 307.966° NW | 2025-07-19 10:49:16.531Z | 359.055° N | 34.378° | 2025-07-19 10:54:16.531Z | 86.764° E |
8 mins | 2025-07-19 12:29:16.531Z | 292.683° NW | 2025-07-19 12:33:16.531Z | 198.285° SSW | 42.603° | 2025-07-19 12:37:16.531Z | 132.084° SE |
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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