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, 10.3 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 112
1 41184U 15081F 25309.09792075 .00001018 00000-0 25327-3 0 9993
2 41184 46.9989 249.5638 0002139 279.6344 80.4299 14.58533744526236Epoch: 2025-11-05T02:21Z
TLE epoch observation values (Epoch: 2025-11-05T02:21:00.352Z)
Latitude
-0.0001°
Longitude
169.73677°
Altitude
697.876 km
Speed
7.509 km/s
True Right ascension
16h 38m 15s
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
07:30:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
700.661 km
Perigee altitude
697.634 km
Semi-major axis
7,077.284 km
Eccentricity
0.00021
Inclination
46.9989°
RAAN
249.5638°
Arg. of periapsis
279.6344°
True anomaly
80.45407°
Mean anomaly
80.4299°
Eccentric anomaly
80.44199°
Mean motion
3.64538 °/min
Orbital period
98.76 mins
BSTAR
0.00025327
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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 | 2025-11-05 22:13:38.203Z | 194.215° SSW | 2025-11-05 22:17:38.203Z | 139.308° SSE | 24.668° | 2025-11-05 22:21:38.203Z | 82.031° E |
| 8 mins | 2025-11-05 23:57:38.203Z | 250.473° W | 2025-11-06 00:00:38.203Z | 301.418° NW | 43.801° | 2025-11-06 00:05:38.203Z | 60.155° ENE |
| 7 mins | 2025-11-06 01:41:38.203Z | 293.811° NW | 2025-11-06 01:44:38.203Z | 346.432° N | 31.316° | 2025-11-06 01:48:38.203Z | 57.049° ENE |
| 8 mins | 2025-11-06 03:25:38.203Z | 307.634° NW | 2025-11-06 03:28:38.203Z | 357.04° N | 34.241° | 2025-11-06 03:33:38.203Z | 85.762° E |
| 8 mins | 2025-11-06 05:09:38.203Z | 291.478° WNW | 2025-11-06 05:12:38.203Z | 231.146° WSW | 42.936° | 2025-11-06 05:17:38.203Z | 130.138° 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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