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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Edit Public Description
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, 6.5 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 111
1 40089U 14040D 25260.23057819 .00002467 00000-0 29570-3 0 9995
2 40089 47.0019 314.8496 0031024 273.7637 85.9713 14.86806335603921Epoch: 2025-09-17T05:32Z
TLE epoch observation values (Epoch: 2025-09-17T05:32:01.955Z)
Latitude
-0.00002°
Longitude
-124.56807°
Altitude
606.684 km
Speed
7.558 km/s
True Right ascension
20h 59m 23s
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
13:32:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.85 km
Perigee altitude
587.495 km
Semi-major axis
6,987.309 km
Eccentricity
0.0031
Inclination
47.0019°
RAAN
314.8496°
Arg. of periapsis
273.7637°
True anomaly
86.32602°
Mean anomaly
85.9713°
Eccentric anomaly
86.14865°
Mean motion
3.71602 °/min
Orbital period
96.88 mins
BSTAR
0.0002957
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 05:53:34.072Z | 192.541° SSW | 2025-09-18 05:56:34.072Z | 141.725° SSE | 25.727° | 2025-09-18 06:00:34.072Z | 79.658° E |
| 7 mins | 2025-09-18 07:34:34.072Z | 254.745° W | 2025-09-18 07:37:34.072Z | 305.911° NW | 42.183° | 2025-09-18 07:41:34.072Z | 57.285° ENE |
| 6 mins | 2025-09-18 09:17:34.072Z | 304.703° NW | 2025-09-18 09:19:34.072Z | 345.96° N | 29.179° | 2025-09-18 09:23:34.072Z | 57.814° ENE |
| 6 mins | 2025-09-18 10:59:34.072Z | 315.661° NNW | 2025-09-18 11:01:34.072Z | 357.286° N | 33.29° | 2025-09-18 11:05:34.072Z | 82.412° E |
| 7 mins | 2025-09-18 12:40:34.072Z | 290.643° WNW | 2025-09-18 12:43:34.072Z | 223.976° SW | 42.197° | 2025-09-18 12:47:34.072Z | 132.844° SE |
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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