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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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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 112
1 41925U 17003J 26089.08581288 .00000011 00000-0 -31283-5 0 9992
2 41925 86.3942 121.3905 0002030 90.5278 269.6150 14.34217576481936Epoch: 2026-03-30T02:03Z
TLE epoch observation values (Epoch: 2026-03-30T02:03:34.232Z)
Latitude
-0.00009°
Longitude
-96.98455°
Altitude
780.729 km
Speed
7.463 km/s
True Right ascension
08h 05m 33s
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
16:10:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.084 km
Perigee altitude
773.18 km
Semi-major axis
7,152.769 km
Eccentricity
0.0002
Inclination
86.3942°
RAAN
121.3905°
Arg. of periapsis
90.5278°
True anomaly
269.59174°
Mean anomaly
269.615°
Eccentric anomaly
269.60337°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000031283
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-30 14:22:17.353Z | 354.535° N | 2026-03-30 14:26:17.353Z | 209.928° SW | 43.883° | 2026-03-30 14:30:17.353Z | 182.947° SSW |
| 6 mins | 2026-03-31 01:39:17.353Z | 115.009° SE | 2026-03-31 01:41:17.353Z | 84.112° E | 21.583° | 2026-03-31 01:45:17.353Z | 31.753° NE |
| 8 mins | 2026-03-31 03:18:17.353Z | 217.57° SW | 2026-03-31 03:22:17.353Z | 289.034° WNW | 30.897° | 2026-03-31 03:26:17.353Z | 343.772° N |
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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