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
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: 1 day ago
TLE from 1 day ago
0 ORBCOMM FM 109
1 40086U 14040A 26082.21210124 .00000469 00000-0 13572-3 0 9998
2 40086 47.0023 137.9396 0002103 215.9176 144.1569 14.58742817621793Epoch: 2026-03-23T05:05Z
TLE epoch observation values (Epoch: 2026-03-23T05:05:25.547Z)
Latitude
0.00002°
Longitude
-119.12418°
Altitude
698.658 km
Speed
7.508 km/s
True Right ascension
09h 11m 45s
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
10:40:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.959 km
Perigee altitude
696.983 km
Semi-major axis
7,076.608 km
Eccentricity
0.00021
Inclination
47.0023°
RAAN
137.9396°
Arg. of periapsis
215.9176°
True anomaly
144.17101°
Mean anomaly
144.1569°
Eccentric anomaly
144.16395°
Mean motion
3.64591 °/min
Orbital period
98.74 mins
BSTAR
0.00013572
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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 | 2026-03-24 05:54:13.604Z | 203.554° SW | 2026-03-24 05:58:13.604Z | 147.65° SSE | 29.553° | 2026-03-24 06:02:13.604Z | 79.803° E |
| 8 mins | 2026-03-24 07:38:13.604Z | 258.232° W | 2026-03-24 07:42:13.604Z | 5.087° NNE | 41.318° | 2026-03-24 07:46:13.604Z | 58.101° ENE |
| 7 mins | 2026-03-24 09:23:13.604Z | 303.611° NW | 2026-03-24 09:26:13.604Z | 6.551° NNE | 30.463° | 2026-03-24 09:30:13.604Z | 62.997° ENE |
| 7 mins | 2026-03-24 11:07:13.604Z | 311.979° NW | 2026-03-24 11:10:13.604Z | 23.843° NE | 36.992° | 2026-03-24 11:14:13.604Z | 90.048° ESE |
| 8 mins | 2026-03-24 12:50:13.604Z | 287.231° WNW | 2026-03-24 12:53:13.604Z | 235.932° WSW | 38.86° | 2026-03-24 12:58:13.604Z | 138.708° SSE |
| 5 mins | 2026-03-25 04:56:13.604Z | 158.76° S | 2026-03-25 04:58:13.604Z | 127.666° SE | 18.309° | 2026-03-25 05:01:13.604Z | 90.008° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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