ORBCOMM FM 112, 41184
Orbit data source: Space-Track
ORBCOMM FM 112, 41184 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Tue, 22 Dec 2015 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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41184 intel report (Beta)
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Edit Public Description
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, 6.5 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 ORBCOMM FM 112
1 41184U 15081F 25257.37628063 .00000586 00000-0 16176-3 0 9992
2 41184 46.9985 133.9701 0001375 18.8560 341.2376 14.58384114518682Epoch: 2025-09-14T09:01Z
TLE epoch observation values (Epoch: 2025-09-14T09:01:50.646Z)
Latitude
-0.00004°
Longitude
4.91287°
Altitude
697.69 km
Speed
7.509 km/s
True Right ascension
08h 55m 52s
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
00:42:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.605 km
Perigee altitude
698.658 km
Semi-major axis
7,077.768 km
Eccentricity
0.00014
Inclination
46.9985°
RAAN
133.9701°
Arg. of periapsis
18.856°
True anomaly
341.23253°
Mean anomaly
341.2376°
Eccentric anomaly
341.23507°
Mean motion
3.64501 °/min
Orbital period
98.77 mins
BSTAR
0.00016176
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Other satellites on launch #81 in the year 2015 (2015-12-22 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 112 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 | 2025-09-15 18:04:41.241Z | 205.326° SW | 2025-09-15 18:08:41.241Z | 143.557° SSE | 31.41° | 2025-09-15 18:12:41.241Z | 77.295° E |
| 8 mins | 2025-09-15 19:48:41.241Z | 261.387° W | 2025-09-15 19:51:41.241Z | 309.825° NW | 40.304° | 2025-09-15 19:56:41.241Z | 58.059° ENE |
| 7 mins | 2025-09-15 21:33:41.241Z | 305.662° NW | 2025-09-15 21:36:41.241Z | 9.542° NNE | 30.22° | 2025-09-15 21:40:41.241Z | 64.347° ENE |
| 8 mins | 2025-09-15 23:16:41.241Z | 305.738° NW | 2025-09-15 23:20:41.241Z | 28.162° NE | 37.743° | 2025-09-15 23:24:41.241Z | 92.457° ESE |
| 8 mins | 2025-09-16 01:00:41.241Z | 285.096° WNW | 2025-09-16 01:03:41.241Z | 230.67° WSW | 37.604° | 2025-09-16 01:08:41.241Z | 141.3° SSE |
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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