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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Identifier
Orbit
Country
US / ORBRelated business
Manufacturer
SNC Louisville
Mission
Partially 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, 5.3 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 26262.81400723 .00000200 00000-0 78402-4 0 9997
2 40086 47.0047 4.0705 0002153 277.9096 82.1545 14.58921695648169Epoch: 2026-09-19T19:32Z
TLE epoch observation values (Epoch: 2026-09-19T19:32:10.224Z)
Latitude
-0.00006°
Longitude
72.3107°
Altitude
696.666 km
Speed
7.509 km/s
True Right ascension
00h 16m 16s
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
03:56:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.416 km
Perigee altitude
696.369 km
Semi-major axis
7,076.029 km
Eccentricity
0.00022
Inclination
47.0047°
RAAN
4.0705°
Arg. of periapsis
277.9096°
True anomaly
82.17894°
Mean anomaly
82.1545°
Eccentric anomaly
82.16672°
Mean motion
3.64635 °/min
Orbital period
98.73 mins
BSTAR
0.000078402
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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 | 2026-09-20 12:16:07.735Z | 283.154° WNW | 2026-09-20 12:20:07.735Z | 338.212° N | 38.039° | 2026-09-20 12:25:07.735Z | 59.916° ENE |
| 8 mins | 2026-09-20 14:01:07.735Z | 306.315° NW | 2026-09-20 14:05:07.735Z | 22.365° NNE | 40.779° | 2026-09-20 14:09:07.735Z | 80.781° E |
| 8 mins | 2026-09-20 15:45:07.735Z | 295.91° NW | 2026-09-20 15:48:07.735Z | 271.875° WNW | 72.235° | 2026-09-20 15:53:07.735Z | 124.278° SE |
| 5 mins | 2026-09-20 17:29:07.735Z | 259.262° W | 2026-09-20 17:31:07.735Z | 232.04° WSW | 18.217° | 2026-09-20 17:34:07.735Z | 190.41° SSW |
| 8 mins | 2026-09-21 09:32:07.735Z | 220.102° SW | 2026-09-21 09:35:07.735Z | 169.795° S | 57.43° | 2026-09-21 09:40:07.735Z | 67.474° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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