ORBCOMM FM 116, 41189
Orbit data source: Space-Track
ORBCOMM FM 116, 41189 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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41189 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, 6.5 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ORBCOMM FM 116
1 41189U 15081L 25261.03005000 .00000666 00000-0 17888-3 0 9995
2 41189 47.0015 117.0115 0002005 237.3481 122.7211 14.58383971519205Epoch: 2025-09-18T00:43Z
TLE epoch observation values (Epoch: 2025-09-18T00:43:16.32Z)
Latitude
-0.00002°
Longitude
108.99598°
Altitude
699.379 km
Speed
7.507 km/s
True Right ascension
07h 48m 02s
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
21:17:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
701.05 km
Perigee altitude
698.212 km
Semi-major axis
7,077.768 km
Eccentricity
0.0002
Inclination
47.0015°
RAAN
117.0115°
Arg. of periapsis
237.3481°
True anomaly
122.74043°
Mean anomaly
122.7211°
Eccentric anomaly
122.73076°
Mean motion
3.64501 °/min
Orbital period
98.77 mins
BSTAR
0.00017888
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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 116 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 16:20:53.014Z | 191.38° SSW | 2025-09-19 16:23:53.014Z | 145.234° SSE | 26.335° | 2025-09-19 16:27:53.014Z | 82.304° E |
| 8 mins | 2025-09-19 18:03:53.014Z | 253.046° W | 2025-09-19 18:07:53.014Z | 15.811° NNE | 42.46° | 2025-09-19 18:11:53.014Z | 59.147° ENE |
| 8 mins | 2025-09-19 19:47:53.014Z | 292.909° NW | 2025-09-19 19:51:53.014Z | 6.985° NNE | 30.731° | 2025-09-19 19:55:53.014Z | 61.801° ENE |
| 7 mins | 2025-09-19 21:32:53.014Z | 312.746° NW | 2025-09-19 21:35:53.014Z | 22.324° NNE | 35.549° | 2025-09-19 21:39:53.014Z | 86.347° E |
| 8 mins | 2025-09-19 23:15:53.014Z | 290.612° WNW | 2025-09-19 23:18:53.014Z | 245.944° WSW | 40.937° | 2025-09-19 23:23:53.014Z | 133.597° 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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