ORBCOMM FM 113, 41185
Orbit data source: Space-Track
ORBCOMM FM 113, 41185 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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41185 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ORBCOMM FM 113
1 41185U 15081G 26163.05131900 .00000335 00000-0 10705-3 0 9998
2 41185 47.0017 294.9070 0001998 204.7602 155.3188 14.58853293558185Epoch: 2026-06-12T01:13Z
TLE epoch observation values (Epoch: 2026-06-12T01:13:53.961Z)
Latitude
-0.00004°
Longitude
16.04581°
Altitude
698.379 km
Speed
7.508 km/s
True Right ascension
19h 39m 37s
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
20:02:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
699.528 km
Perigee altitude
696.7 km
Semi-major axis
7,076.251 km
Eccentricity
0.0002
Inclination
47.0017°
RAAN
294.907°
Arg. of periapsis
204.7602°
True anomaly
155.32836°
Mean anomaly
155.3188°
Eccentric anomaly
155.32358°
Mean motion
3.64618 °/min
Orbital period
98.73 mins
BSTAR
0.00010705
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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 113 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-13 10:15:47.064Z | 169.868° S | 2026-06-13 10:18:47.064Z | 127.593° SE | 17.617° | 2026-06-13 10:20:47.064Z | 100.238° ESE |
| 8 mins | 2026-06-13 11:57:47.064Z | 235.71° WSW | 2026-06-13 12:01:47.064Z | 84.735° E | 43.565° | 2026-06-13 12:05:47.064Z | 63.291° ENE |
| 8 mins | 2026-06-13 13:41:47.064Z | 285.627° WNW | 2026-06-13 13:44:47.064Z | 338.217° N | 33.079° | 2026-06-13 13:49:47.064Z | 59.458° ENE |
| 8 mins | 2026-06-13 15:25:47.064Z | 305.823° NW | 2026-06-13 15:29:47.064Z | 22.776° NE | 31.839° | 2026-06-13 15:33:47.064Z | 77.725° E |
| 8 mins | 2026-06-13 17:09:47.064Z | 298.916° NW | 2026-06-13 17:12:47.064Z | 307.818° NW | 44.015° | 2026-06-13 17:17:47.064Z | 118.166° SE |
| 6 mins | 2026-06-13 18:53:47.064Z | 262.032° W | 2026-06-13 18:55:47.064Z | 232.496° WSW | 20.482° | 2026-06-13 18:59:47.064Z | 176.182° S |
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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