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IRIDIUM 108, 41924

Orbit data source: Space-Track

IRIDIUM 108, 41924 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
41924, 2017-003H
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 (10 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: 20 hours ago

TLE from 20 hours ago
0 IRIDIUM 108
1 41924U 17003H   26229.84988709 -.00000021  00000-0 -14465-4 0  9994
2 41924  86.3951  30.9607 0001994  90.3846 269.7578 14.34217435503941
Epoch: 2026-08-17T20:23Z
TLE epoch observation values (Epoch: 2026-08-17T20:23:50.244Z)
Latitude
-0.00006°
Longitude
118.7752°
Altitude
780.725 km
Speed
7.463 km/s
True Right ascension
02h 03m 50s
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
07:06:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.059 km
Perigee altitude
773.206 km
Semi-major axis
7,152.77 km
Eccentricity
0.0002
Inclination
86.3951°
RAAN
30.9607°
Arg. of periapsis
90.3846°
True anomaly
269.73495°
Mean anomaly
269.7578°
Eccentric anomaly
269.74638°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000014465
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