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: 15 hours ago
TLE from 15 hours ago
0 IRIDIUM 112
1 41925U 17003J 26125.01659786 .00000117 00000-0 34860-4 0 9994
2 41925 86.3928 106.3586 0002248 91.0801 269.0652 14.34218765487081Epoch: 2026-05-05T00:23Z
TLE epoch observation values (Epoch: 2026-05-05T00:23:54.055Z)
Latitude
-0.00004°
Longitude
-122.51412°
Altitude
780.741 km
Speed
7.463 km/s
True Right ascension
07h 05m 26s
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
23:14:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.236 km
Perigee altitude
773.02 km
Semi-major axis
7,152.765 km
Eccentricity
0.00022
Inclination
86.3928°
RAAN
106.3586°
Arg. of periapsis
91.0801°
True anomaly
269.03944°
Mean anomaly
269.0652°
Eccentric anomaly
269.05232°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.00003486
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-05 22:17:57.164Z | 128.231° SE | 2026-05-05 22:20:57.164Z | 87.741° E | 21.973° | 2026-05-05 22:24:57.164Z | 32.827° NE |
| 7 mins | 2026-05-05 23:58:57.164Z | 225.458° WSW | 2026-05-06 00:01:57.164Z | 283.511° WNW | 30.566° | 2026-05-06 00:05:57.164Z | 342.092° N |
| 8 mins | 2026-05-06 10:28:57.164Z | 14.096° NNE | 2026-05-06 10:31:57.164Z | 73.765° E | 39.236° | 2026-05-06 10:36:57.164Z | 161.987° S |
| 4 mins | 2026-05-06 12:10:57.164Z | 300° NW | 2026-05-06 12:11:57.164Z | 286.895° WNW | 15.29° | 2026-05-06 12:14:57.164Z | 249.202° W |
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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