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, 10.3 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ORBCOMM FM 109
1 40086U 14040A 25348.16594614 .00000967 00000-0 24234-3 0 9995
2 40086 47.0029 246.0777 0001139 76.9869 283.1144 14.58547557607337Epoch: 2025-12-14T03:58Z
TLE epoch observation values (Epoch: 2025-12-14T03:58:57.746Z)
Latitude
-0°
Longitude
103.25432°
Altitude
697.901 km
Speed
7.509 km/s
True Right ascension
16h 24m 18s
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
17:52:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.908 km
Perigee altitude
698.296 km
Semi-major axis
7,077.239 km
Eccentricity
0.00011
Inclination
47.0029°
RAAN
246.0777°
Arg. of periapsis
76.9869°
True anomaly
283.10169°
Mean anomaly
283.1144°
Eccentric anomaly
283.10804°
Mean motion
3.64542 °/min
Orbital period
98.75 mins
BSTAR
0.00024234
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-14 20:36:18.868Z | 231.313° WSW | 2025-12-14 20:41:18.868Z | 139.447° SSE | 43.524° | 2025-12-14 20:45:18.868Z | 65.795° ENE |
| 8 mins | 2025-12-14 22:21:18.868Z | 279.555° WNW | 2025-12-14 22:25:18.868Z | 358.47° N | 34.204° | 2025-12-14 22:29:18.868Z | 57.201° ENE |
| 7 mins | 2025-12-15 00:06:18.868Z | 310.084° NW | 2025-12-15 00:09:18.868Z | 10.046° NNE | 31.523° | 2025-12-15 00:13:18.868Z | 72.812° E |
| 8 mins | 2025-12-15 01:49:18.868Z | 300.711° NW | 2025-12-15 01:53:18.868Z | 48.437° ENE | 44.274° | 2025-12-15 01:57:18.868Z | 112.465° ESE |
| 7 mins | 2025-12-15 03:33:18.868Z | 270.051° WNW | 2025-12-15 03:36:18.868Z | 223.042° SW | 23.87° | 2025-12-15 03:40:18.868Z | 167.664° 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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