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: 16 hours ago
TLE from 16 hours ago
0 ORBCOMM FM 111
1 40089U 14040D 26262.78027383 .00001189 00000-0 14707-3 0 9997
2 40089 47.0012 294.1954 0029081 240.8690 118.9296 14.89187307658676Epoch: 2026-09-19T18:43Z
TLE epoch observation values (Epoch: 2026-09-19T18:43:35.658Z)
Latitude
-0.00005°
Longitude
14.61288°
Altitude
610.553 km
Speed
7.55 km/s
True Right ascension
19h 36m 46s
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
03:56:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.023 km
Perigee altitude
581.427 km
Semi-major axis
6,979.862 km
Eccentricity
0.00291
Inclination
47.0012°
RAAN
294.1954°
Arg. of periapsis
240.869°
True anomaly
119.22075°
Mean anomaly
118.9296°
Eccentric anomaly
119.07522°
Mean motion
3.72197 °/min
Orbital period
96.72 mins
BSTAR
0.00014707
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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 | 2026-09-20 11:18:40.461Z | 294.142° NW | 2026-09-20 11:22:40.461Z | 209.616° SW | 69.345° | 2026-09-20 11:26:40.461Z | 130.187° SE |
| 7 mins | 2026-09-21 04:43:40.461Z | 211.79° SW | 2026-09-21 04:46:40.461Z | 151.4° SSE | 47.315° | 2026-09-21 04:50:40.461Z | 72.336° E |
| 6 mins | 2026-09-21 06:25:40.461Z | 276.469° WNW | 2026-09-21 06:27:40.461Z | 318.97° NNW | 46.975° | 2026-09-21 06:31:40.461Z | 53.034° ENE |
| 6 mins | 2026-09-21 08:07:40.461Z | 310.324° NW | 2026-09-21 08:09:40.461Z | 348.738° N | 32.161° | 2026-09-21 08:13:40.461Z | 62.026° ENE |
| 7 mins | 2026-09-21 09:48:40.461Z | 307.044° NW | 2026-09-21 09:51:40.461Z | 2.001° NNE | 51.835° | 2026-09-21 09:55:40.461Z | 95.451° ESE |
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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