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, 5.3 m
Radar Cross Section
2.222 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 ORBCOMM FM 112
1 41184U 15081F 26306.47690951 .00000317 00000-0 10300-3 0 9999
2 41184 46.9998 336.2535 0001904 145.9701 214.1307 14.59006751579145Epoch: 2026-11-02T11:26Z
TLE epoch observation values (Epoch: 2026-11-02T11:26:44.981Z)
Latitude
-0.00004°
Longitude
122.81267°
Altitude
697.713 km
Speed
7.508 km/s
True Right ascension
22h 25m 00s
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
06:09:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.965 km
Perigee altitude
696.271 km
Semi-major axis
7,075.755 km
Eccentricity
0.00019
Inclination
46.9998°
RAAN
336.2535°
Arg. of periapsis
145.9701°
True anomaly
214.11846°
Mean anomaly
214.1307°
Eccentric anomaly
214.12458°
Mean motion
3.64657 °/min
Orbital period
98.72 mins
BSTAR
0.000103
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-03 10:55:22.375Z | 297.106° NW | 2026-11-03 11:00:22.375Z | 173.747° S | 81.204° | 2026-11-03 11:04:22.375Z | 123.588° SE |
| 5 mins | 2026-11-03 12:41:22.375Z | 252.299° W | 2026-11-03 12:43:22.375Z | 222.362° SW | 18.743° | 2026-11-03 12:46:22.375Z | 183.812° SSW |
| 8 mins | 2026-11-04 04:43:22.375Z | 220.327° SW | 2026-11-04 04:47:22.375Z | 131.712° SE | 57.529° | 2026-11-04 04:51:22.375Z | 68.754° E |
| 8 mins | 2026-11-04 06:27:22.375Z | 275.606° WNW | 2026-11-04 06:30:22.375Z | 329.824° NNW | 47.021° | 2026-11-04 06:35:22.375Z | 57.673° ENE |
| 8 mins | 2026-11-04 08:11:22.375Z | 302.915° NW | 2026-11-04 08:15:22.375Z | 16.877° NNE | 35.551° | 2026-11-04 08:19:22.375Z | 70.442° E |
| 8 mins | 2026-11-04 09:55:22.375Z | 304.391° NW | 2026-11-04 09:59:22.375Z | 54.675° ENE | 61.866° | 2026-11-04 10:03:22.375Z | 105.045° ESE |
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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