Showing default

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.

Loading next visibility...
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 (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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 IRIDIUM 108
1 41924U 17003H   25260.79822283  .00000053  00000-0  11838-4 0  9990
2 41924  86.4040 170.6044 0002256  79.4799 280.6651 14.34218092456069
Epoch: 2025-09-17T19:09Z
TLE epoch observation values (Epoch: 2025-09-17T19:09:26.452Z)
Latitude
-0.00002°
Longitude
-113.72482°
Altitude
780.419 km
Speed
7.464 km/s
True Right ascension
11h 22m 25s
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
16:47:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.244 km
Perigee altitude
773.017 km
Semi-major axis
7,152.767 km
Eccentricity
0.00023
Inclination
86.404°
RAAN
170.6044°
Arg. of periapsis
79.4799°
True anomaly
280.63969°
Mean anomaly
280.6651°
Eccentric anomaly
280.6524°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000011838
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|