ORBCOMM FM 109, 40086
Orbit data source: Space-Track
ORBCOMM FM 109, 40086 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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40086 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
US / ORBRelated business
Manufacturer
SNC Louisville
Mission
Operational Commercial Communications
Bus & Motor
SN-100A, Unknown motor
Mass
172 kg wet, 158 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 6.5 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ORBCOMM FM 109
1 40086U 14040A 25260.13411296 .00000411 00000-0 12449-3 0 9998
2 40086 47.0035 302.0056 0001110 2.4455 357.6436 14.58301584594481Epoch: 2025-09-17T03:13Z
TLE epoch observation values (Epoch: 2025-09-17T03:13:07.359Z)
Latitude
-0.00002°
Longitude
-102.58951°
Altitude
698.094 km
Speed
7.509 km/s
True Right ascension
20h 08m 01s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:33:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.683 km
Perigee altitude
699.112 km
Semi-major axis
7,078.035 km
Eccentricity
0.00011
Inclination
47.0035°
RAAN
302.0056°
Arg. of periapsis
2.4455°
True anomaly
357.64308°
Mean anomaly
357.6436°
Eccentric anomaly
357.64334°
Mean motion
3.6448 °/min
Orbital period
98.77 mins
BSTAR
0.00012449
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Other satellites on launch #40 in the year 2014 (2014-07-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ORBCOMM FM 109 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-18 05:43:13.551Z | 219.884° SW | 2025-09-18 05:47:13.551Z | 123.144° SE | 39.733° | 2025-09-18 05:51:13.551Z | 68.382° E |
| 8 mins | 2025-09-18 07:27:13.551Z | 276.372° WNW | 2025-09-18 07:30:13.551Z | 334.288° NNW | 36.424° | 2025-09-18 07:35:13.551Z | 58.353° ENE |
| 8 mins | 2025-09-18 09:11:13.551Z | 303.263° NW | 2025-09-18 09:14:13.551Z | 351.071° N | 30.375° | 2025-09-18 09:19:13.551Z | 71.224° E |
| 8 mins | 2025-09-18 10:55:13.551Z | 303.999° NW | 2025-09-18 10:59:13.551Z | 57.684° ENE | 41.565° | 2025-09-18 11:03:13.551Z | 105.78° ESE |
| 7 mins | 2025-09-18 12:39:13.551Z | 272.169° WNW | 2025-09-18 12:42:13.551Z | 216.409° SW | 28.595° | 2025-09-18 12:46:13.551Z | 158.896° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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