ORBCOMM FM 104, 40090
Orbit data source: Space-Track
ORBCOMM FM 104, 40090 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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40090 intel report (Beta)
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TLE from 1 day ago
0 ORBCOMM FM 104
1 40090U 14040E 25198.24464790 .00000286 00000-0 10119-3 0 9994
2 40090 47.0049 269.2589 0016524 338.5885 21.4307 14.56676152585006
TLE epoch observation values (Epoch: 2025-07-17T05:52:17.578Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #40 in the year 2014 (2014-07-14 UTC)
ORBCOMM FM 104 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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9 mins | 2025-07-18 08:25:21.052Z | 247.201° WSW | 2025-07-18 08:30:21.052Z | 16.72° NNE | 43.762° | 2025-07-18 08:34:21.052Z | 59.837° ENE |
7 mins | 2025-07-18 10:11:21.052Z | 297.552° NW | 2025-07-18 10:14:21.052Z | 359.665° N | 31.578° | 2025-07-18 10:18:21.052Z | 59.557° ENE |
7 mins | 2025-07-18 11:55:21.052Z | 309.939° NW | 2025-07-18 11:58:21.052Z | 7.791° NNE | 34.799° | 2025-07-18 12:02:21.052Z | 81.728° E |
8 mins | 2025-07-18 13:39:21.052Z | 291.516° WNW | 2025-07-18 13:42:21.052Z | 216.935° SW | 43.444° | 2025-07-18 13:47:21.052Z | 129.185° SE |
8 mins | 2025-07-19 07:27:21.052Z | 227.986° WSW | 2025-07-19 07:31:21.052Z | 123.861° SE | 42.81° | 2025-07-19 07:35:21.052Z | 66.042° ENE |
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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