ORBCOMM FM 103, 40091
Orbit data source: Space-Track
ORBCOMM FM 103, 40091 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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40091 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 103
1 40091U 14040F 25259.86138447 .00000451 00000-0 13319-3 0 9997
2 40091 47.0057 304.8234 0002282 313.3665 46.7030 14.58301675577485
TLE epoch observation values (Epoch: 2025-09-16T20:40:23.618Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #40 in the year 2014 (2014-07-14 UTC)
ORBCOMM FM 103 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 05:45:05.801Z | 216.606° SW | 2025-09-18 05:48:05.801Z | 166.523° S | 38.529° | 2025-09-18 05:53:05.801Z | 68.823° E |
7 mins | 2025-09-18 07:29:05.801Z | 275.862° WNW | 2025-09-18 07:32:05.801Z | 340.882° N | 37.223° | 2025-09-18 07:36:05.801Z | 54.975° ENE |
7 mins | 2025-09-18 09:13:05.801Z | 304.148° NW | 2025-09-18 09:16:05.801Z | 355.678° N | 30.581° | 2025-09-18 09:20:05.801Z | 65.488° ENE |
8 mins | 2025-09-18 10:57:05.801Z | 305.297° NW | 2025-09-18 11:00:05.801Z | 358.215° N | 41.366° | 2025-09-18 11:05:05.801Z | 104.288° ESE |
7 mins | 2025-09-18 12:41:05.801Z | 272.055° WNW | 2025-09-18 12:44:05.801Z | 211.896° SW | 29.844° | 2025-09-18 12:48:05.801Z | 155.983° 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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