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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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: 16 hours ago
TLE from 16 hours ago
0 ORBCOMM FM 112
1 41184U 15081F 26048.21554382 .00000913 00000-0 23022-3 0 9998
2 41184 46.9984 117.4473 0001736 337.8976 22.1835 14.58690772541434Epoch: 2026-02-17T05:10Z
TLE epoch observation values (Epoch: 2026-02-17T05:10:22.986Z)
Latitude
0.00003°
Longitude
-107.34718°
Altitude
696.482 km
Speed
7.51 km/s
True Right ascension
07h 49m 47s
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
00:28:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.868 km
Perigee altitude
697.411 km
Semi-major axis
7,076.777 km
Eccentricity
0.00017
Inclination
46.9984°
RAAN
117.4473°
Arg. of periapsis
337.8976°
True anomaly
22.19101°
Mean anomaly
22.1835°
Eccentric anomaly
22.18726°
Mean motion
3.64578 °/min
Orbital period
98.74 mins
BSTAR
0.00023022
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-18 05:59:18.815Z | 164° S | 2026-02-18 06:01:18.815Z | 137.78° SSE | 15.77° | 2026-02-18 06:04:18.815Z | 98.357° ESE |
| 8 mins | 2026-02-18 07:41:18.815Z | 230.597° WSW | 2026-02-18 07:44:18.815Z | 173.846° S | 43.833° | 2026-02-18 07:49:18.815Z | 64.259° ENE |
| 7 mins | 2026-02-18 09:25:18.815Z | 285.965° WNW | 2026-02-18 09:28:18.815Z | 348.821° N | 34.138° | 2026-02-18 09:32:18.815Z | 55.92° ENE |
| 7 mins | 2026-02-18 11:09:18.815Z | 307.863° NW | 2026-02-18 11:12:18.815Z | 2.068° NNE | 31.724° | 2026-02-18 11:16:18.815Z | 72.045° E |
| 8 mins | 2026-02-18 12:53:18.815Z | 301.109° NW | 2026-02-18 12:56:18.815Z | 1.303° NNE | 44.571° | 2026-02-18 13:01:18.815Z | 114.918° SE |
| 6 mins | 2026-02-18 14:37:18.815Z | 260.728° W | 2026-02-18 14:39:18.815Z | 227.854° WSW | 22.777° | 2026-02-18 14:43:18.815Z | 170.975° S |
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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