ORBCOMM FM 110, 41182
Orbit data source: Space-Track
ORBCOMM FM 110, 41182 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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41182 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: 1 day ago
TLE from 1 day ago
0 ORBCOMM FM 110
1 41182U 15081D 26237.40942305 .00000414 00000-0 12354-3 0 9995
2 41182 47.0027 34.1144 0002359 29.5257 330.5762 14.58966289567736Epoch: 2026-08-25T09:49Z
TLE epoch observation values (Epoch: 2026-08-25T09:49:34.151Z)
Latitude
-0°
Longitude
-86.95508°
Altitude
695.276 km
Speed
7.511 km/s
True Right ascension
02h 16m 27s
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
09:54:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.418 km
Perigee altitude
696.079 km
Semi-major axis
7,075.885 km
Eccentricity
0.00024
Inclination
47.0027°
RAAN
34.1144°
Arg. of periapsis
29.5257°
True anomaly
330.56292°
Mean anomaly
330.5762°
Eccentric anomaly
330.56956°
Mean motion
3.64646 °/min
Orbital period
98.73 mins
BSTAR
0.00012354
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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 110 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 | 2026-08-26 19:10:32.293Z | 296.533° NW | 2026-08-26 19:14:32.293Z | 253.302° W | 44.478° | 2026-08-26 19:19:32.293Z | 123.632° SE |
| 5 mins | 2026-08-26 20:55:32.293Z | 256.595° W | 2026-08-26 20:57:32.293Z | 228.098° WSW | 17.652° | 2026-08-26 21:00:32.293Z | 187.418° SSW |
| 8 mins | 2026-08-27 12:58:32.293Z | 217.666° SW | 2026-08-27 13:01:32.293Z | 155.641° SSE | 40.079° | 2026-08-27 13:06:32.293Z | 67.467° ENE |
| 8 mins | 2026-08-27 14:41:32.293Z | 272.934° WNW | 2026-08-27 14:45:32.293Z | 353.261° N | 36.443° | 2026-08-27 14:49:32.293Z | 56.283° ENE |
| 7 mins | 2026-08-27 16:26:32.293Z | 307.595° NW | 2026-08-27 16:29:32.293Z | 5.667° NNE | 30.743° | 2026-08-27 16:33:32.293Z | 68.476° E |
| 7 mins | 2026-08-27 18:10:32.293Z | 306.356° NW | 2026-08-27 18:13:32.293Z | 26.805° NE | 42.437° | 2026-08-27 18:17:32.293Z | 104.441° 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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