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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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Identifier
41925, 2017-003J
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2017-01-14 (9 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 IRIDIUM 112
1 41925U 17003J   25340.29335516  .00000016  00000-0 -12442-5 0  9996
2 41925  86.3985 168.9048 0001936  83.8179 276.3237 14.34217521465626
Epoch: 2025-12-06T07:02Z
TLE epoch observation values (Epoch: 2025-12-06T07:02:25.885Z)
Latitude
-0.00007°
Longitude
-12.02623°
Altitude
780.567 km
Speed
7.464 km/s
True Right ascension
11h 15m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:09:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.017 km
Perigee altitude
773.248 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.3985°
RAAN
168.9048°
Arg. of periapsis
83.8179°
True anomaly
276.30165°
Mean anomaly
276.3237°
Eccentric anomaly
276.31267°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000012442
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