ORBCOMM FM 111, 40089
Orbit data source: Space-Track
ORBCOMM FM 111, 40089 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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40089 intel report (Beta)
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Identifier
Orbit
Country
US / ORBRelated business
Manufacturer
SNC Louisville
Mission
Non-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: 17 hours ago
TLE from 17 hours ago
0 ORBCOMM FM 111
1 40089U 14040D 26128.77739876 .00001693 00000-0 20186-3 0 9992
2 40089 47.0000 238.6769 0029204 312.7104 47.1336 14.88654831638706Epoch: 2026-05-08T18:39Z
TLE epoch observation values (Epoch: 2026-05-08T18:39:27.252Z)
Latitude
0.00001°
Longitude
92.20904°
Altitude
588.521 km
Speed
7.575 km/s
True Right ascension
15h 54m 42s
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
19:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.778 km
Perigee altitude
583 km
Semi-major axis
6,981.526 km
Eccentricity
0.00292
Inclination
47°
RAAN
238.6769°
Arg. of periapsis
312.7104°
True anomaly
47.37949°
Mean anomaly
47.1336°
Eccentric anomaly
47.25648°
Mean motion
3.72064 °/min
Orbital period
96.76 mins
BSTAR
0.00020186
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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 111 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 | 2026-05-09 12:40:11.265Z | 284.066° WNW | 2026-05-09 12:44:11.265Z | 348.895° N | 30.278° | 2026-05-09 12:48:11.265Z | 57.117° ENE |
| 7 mins | 2026-05-09 14:23:11.265Z | 309.378° NW | 2026-05-09 14:26:11.265Z | 7.215° NNE | 31.36° | 2026-05-09 14:30:11.265Z | 77.964° E |
| 7 mins | 2026-05-09 16:05:11.265Z | 296.604° NW | 2026-05-09 16:08:11.265Z | 148.119° SSE | 44.54° | 2026-05-09 16:12:11.265Z | 121.885° SE |
| 4 mins | 2026-05-09 17:47:11.265Z | 251.017° W | 2026-05-09 17:49:11.265Z | 218.663° SW | 17.045° | 2026-05-09 17:51:11.265Z | 189.612° SSW |
| 6 mins | 2026-05-10 09:30:11.265Z | 195.736° SSW | 2026-05-10 09:32:11.265Z | 156.321° SSE | 29.778° | 2026-05-10 09:36:11.265Z | 78.166° E |
| 7 mins | 2026-05-10 11:11:11.265Z | 266.281° W | 2026-05-10 11:14:11.265Z | 358.127° N | 39.413° | 2026-05-10 11:18:11.265Z | 57.602° ENE |
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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