ORBCOMM FM 107, 40087
Orbit data source: Space-Track
ORBCOMM FM 107, 40087 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Mon, 14 Jul 2014 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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40087 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 107
1 40087U 14040B 25260.15801886 .00000448 00000-0 13231-3 0 9999
2 40087 47.0052 302.8196 0001746 305.1856 54.8866 14.58383824594566
TLE epoch observation values (Epoch: 2025-09-17T03:47:32.829Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #40 in the year 2014 (2014-07-14 UTC)
ORBCOMM FM 107 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 | 2025-09-18 08:02:10.911Z | 281.372° WNW | 2025-09-18 08:06:10.911Z | 340.193° N | 32.606° | 2025-09-18 08:10:10.911Z | 54.664° ENE |
8 mins | 2025-09-18 09:47:10.911Z | 306.178° NW | 2025-09-18 09:51:10.911Z | 23.666° NE | 32.379° | 2025-09-18 09:55:10.911Z | 79.256° E |
8 mins | 2025-09-18 11:31:10.911Z | 297.509° NW | 2025-09-18 11:34:10.911Z | 289.847° WNW | 43.947° | 2025-09-18 11:39:10.911Z | 120.886° SE |
6 mins | 2025-09-18 13:15:10.911Z | 261.112° W | 2025-09-18 13:17:10.911Z | 232.847° WSW | 19.043° | 2025-09-18 13:21:10.911Z | 178.813° S |
8 mins | 2025-09-19 05:18:10.911Z | 217.476° SW | 2025-09-19 05:22:10.911Z | 137.745° SSE | 38.771° | 2025-09-19 05:26:10.911Z | 70.484° E |
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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