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, 5.3 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ORBCOMM FM 109
1 40086U 14040A 26129.12828863 .00000301 00000-0 99911-4 0 9992
2 40086 47.0037 276.1481 0000975 29.6250 330.4691 14.58804118628647Epoch: 2026-05-09T03:04Z
TLE epoch observation values (Epoch: 2026-05-09T03:04:44.137Z)
Latitude
-0.00002°
Longitude
3.01401°
Altitude
696.654 km
Speed
7.51 km/s
True Right ascension
18h 24m 35s
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
19:56:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.962 km
Perigee altitude
697.583 km
Semi-major axis
7,076.409 km
Eccentricity
0.0001
Inclination
47.0037°
RAAN
276.1481°
Arg. of periapsis
29.625°
True anomaly
330.46359°
Mean anomaly
330.4691°
Eccentric anomaly
330.46635°
Mean motion
3.64606 °/min
Orbital period
98.74 mins
BSTAR
0.000099911
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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 | 2026-05-09 13:07:39.381Z | 231.04° WSW | 2026-05-09 13:12:39.381Z | 116.386° SE | 43.041° | 2026-05-09 13:16:39.381Z | 65.412° ENE |
| 8 mins | 2026-05-09 14:52:39.381Z | 281.262° WNW | 2026-05-09 14:55:39.381Z | 332.842° NNW | 34.081° | 2026-05-09 15:00:39.381Z | 58.365° ENE |
| 7 mins | 2026-05-09 16:37:39.381Z | 312.934° NW | 2026-05-09 16:40:39.381Z | 18.213° NNE | 31.191° | 2026-05-09 16:44:39.381Z | 74.34° E |
| 8 mins | 2026-05-09 18:20:39.381Z | 301.204° NW | 2026-05-09 18:24:39.381Z | 78.391° E | 43.394° | 2026-05-09 18:28:39.381Z | 112.819° SE |
| 6 mins | 2026-05-09 20:04:39.381Z | 266.864° W | 2026-05-09 20:07:39.381Z | 216.567° SW | 23.743° | 2026-05-09 20:10:39.381Z | 172.893° 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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