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: 10 hours ago
TLE from 10 hours ago
0 IRIDIUM 112
1 41925U 17003J 26305.22868344 .00000063 00000-0 15559-4 0 9993
2 41925 86.3998 30.9829 0002083 94.1345 266.0089 14.34217338512911Epoch: 2026-11-01T05:29Z
TLE epoch observation values (Epoch: 2026-11-01T05:29:18.249Z)
Latitude
0°
Longitude
-91.8662°
Altitude
780.824 km
Speed
7.463 km/s
True Right ascension
02h 03m 55s
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
11:33:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.123 km
Perigee altitude
773.143 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3998°
RAAN
30.9829°
Arg. of periapsis
94.1345°
True anomaly
265.98509°
Mean anomaly
266.0089°
Eccentric anomaly
265.99699°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000015559
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-01 17:46:23.408Z | 3.887° NNE | 2026-11-01 17:51:23.408Z | 73.602° E | 63.376° | 2026-11-01 17:56:23.408Z | 166.831° S |
| 9 mins | 2026-11-02 06:43:23.408Z | 197.854° SSW | 2026-11-02 06:47:23.408Z | 270.279° WNW | 59.272° | 2026-11-02 06:52:23.408Z | 354.193° N |
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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