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: 21 hours ago
TLE from 21 hours ago
0 ORBCOMM FM 112
1 41184U 15081F 25357.80137266 .00000660 00000-0 17669-3 0 9992
2 41184 47.0000 19.3763 0000885 162.5329 197.5587 14.58596922533340Epoch: 2025-12-23T19:13Z
TLE epoch observation values (Epoch: 2025-12-23T19:13:58.597Z)
Latitude
-0.00005°
Longitude
-1.6978°
Altitude
698.52 km
Speed
7.508 km/s
True Right ascension
01h 17m 30s
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
15:23:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.569 km
Perigee altitude
698.317 km
Semi-major axis
7,077.08 km
Eccentricity
0.00009
Inclination
47°
RAAN
19.3763°
Arg. of periapsis
162.5329°
True anomaly
197.55564°
Mean anomaly
197.5587°
Eccentric anomaly
197.55717°
Mean motion
3.64554 °/min
Orbital period
98.75 mins
BSTAR
0.00017669
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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 | 2025-12-25 04:17:56.796Z | 218.922° SW | 2025-12-25 04:21:56.796Z | 135.872° SSE | 39.46° | 2025-12-25 04:25:56.796Z | 69.749° E |
| 8 mins | 2025-12-25 06:01:56.796Z | 273.862° WNW | 2025-12-25 06:04:56.796Z | 326.024° NNW | 36.486° | 2025-12-25 06:09:56.796Z | 57.637° ENE |
| 7 mins | 2025-12-25 07:46:56.796Z | 310.496° NW | 2025-12-25 07:49:56.796Z | 14.135° NNE | 30.392° | 2025-12-25 07:53:56.796Z | 69.699° E |
| 8 mins | 2025-12-25 09:29:56.796Z | 303.942° NW | 2025-12-25 09:33:56.796Z | 45.963° ENE | 41.629° | 2025-12-25 09:37:56.796Z | 104.027° ESE |
| 7 mins | 2025-12-25 11:13:56.796Z | 274.505° WNW | 2025-12-25 11:16:56.796Z | 219.768° SW | 29.621° | 2025-12-25 11:20:56.796Z | 158.117° S |
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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