IRIDIUM 112, 41925
Orbit data source: Space-Track
IRIDIUM 112, 41925 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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41925 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 IRIDIUM 112
1 41925U 17003J 25314.61854469 -.00000050 00000-0 -24829-4 0 9996
2 41925 86.4010 179.6225 0002139 83.3088 276.8351 14.34217321461943Epoch: 2025-11-10T14:50Z
TLE epoch observation values (Epoch: 2025-11-10T14:50:42.261Z)
Latitude
-0.00003°
Longitude
-93.07045°
Altitude
780.538 km
Speed
7.464 km/s
True Right ascension
11h 58m 29s
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
09:43:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.163 km
Perigee altitude
773.103 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.401°
RAAN
179.6225°
Arg. of periapsis
83.3088°
True anomaly
276.81076°
Mean anomaly
276.8351°
Eccentric anomaly
276.82293°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000024829
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Other satellites on launch #3 in the year 2017 (2017-01-14 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.IRIDIUM 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-11 14:26:27.357Z | 108.106° ESE | 2025-11-11 14:28:27.357Z | 82.563° E | 15.954° | 2025-11-11 14:31:27.357Z | 44.899° NE |
| 8 mins | 2025-11-11 16:05:27.357Z | 204.947° SW | 2025-11-11 16:08:27.357Z | 255.656° W | 37.941° | 2025-11-11 16:13:27.357Z | 350.962° N |
| 7 mins | 2025-11-12 02:36:27.357Z | 27.058° NE | 2025-11-12 02:39:27.357Z | 84.948° E | 31.454° | 2025-11-12 02:43:27.357Z | 146.203° SSE |
| 6 mins | 2025-11-12 04:17:27.357Z | 313.885° NW | 2025-11-12 04:19:27.357Z | 284.31° WNW | 21.286° | 2025-11-12 04:23:27.357Z | 230.106° WSW |
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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