ORBCOMM FM 114, 41179
Orbit data source: Space-Track
ORBCOMM FM 114, 41179 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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41179 intel report (Beta)
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Identifier
Orbit
Country
US / ORBRelated business
Manufacturer
SNC Louisville
Mission
Partially 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ORBCOMM FM 114
1 41179U 15081A 26129.48825786 .00000221 00000-0 82961-4 0 9990
2 41179 47.0036 184.9621 0001941 353.3263 6.7597 14.58815118552104Epoch: 2026-05-09T11:43Z
TLE epoch observation values (Epoch: 2026-05-09T11:43:05.479Z)
Latitude
0.00002°
Longitude
141.88432°
Altitude
695.855 km
Speed
7.51 km/s
True Right ascension
12h 19m 50s
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
06:44:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.61 km
Perigee altitude
696.863 km
Semi-major axis
7,076.374 km
Eccentricity
0.00019
Inclination
47.0036°
RAAN
184.9621°
Arg. of periapsis
353.3263°
True anomaly
6.76232°
Mean anomaly
6.7597°
Eccentric anomaly
6.76101°
Mean motion
3.64609 °/min
Orbital period
98.74 mins
BSTAR
0.000082961
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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 114 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 | 2026-05-10 05:57:05.166Z | 201.188° SSW | 2026-05-10 06:01:05.166Z | 146.909° SSE | 27.901° | 2026-05-10 06:05:05.166Z | 81.129° E |
| 8 mins | 2026-05-10 07:41:05.166Z | 255.788° W | 2026-05-10 07:45:05.166Z | 9.688° NNE | 41.877° | 2026-05-10 07:49:05.166Z | 58.585° ENE |
| 7 mins | 2026-05-10 09:26:05.166Z | 303.044° NW | 2026-05-10 09:29:05.166Z | 7.355° NNE | 30.484° | 2026-05-10 09:33:05.166Z | 62.516° ENE |
| 8 mins | 2026-05-10 11:09:05.166Z | 305.933° NW | 2026-05-10 11:13:05.166Z | 24.716° NE | 36.196° | 2026-05-10 11:17:05.166Z | 88.399° E |
| 8 mins | 2026-05-10 12:53:05.166Z | 288.673° WNW | 2026-05-10 12:56:05.166Z | 237.174° WSW | 40.163° | 2026-05-10 13:01:05.166Z | 136.086° 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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