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IRIDIUM 106, 41917

Orbit data source: Space-Track

IRIDIUM 106, 41917 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
41917, 2017-003A
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: 9 hours ago

TLE from 9 hours ago
0 IRIDIUM 106
1 41917U 17003A   25340.25530341  .00000078  00000-0  20911-4 0  9992
2 41917  86.3988 169.1614 0002124 101.4161 258.7274 14.34219273465553
Epoch: 2025-12-06T06:07Z
TLE epoch observation values (Epoch: 2025-12-06T06:07:38.214Z)
Latitude
0.00002°
Longitude
1.96651°
Altitude
781.011 km
Speed
7.463 km/s
True Right ascension
11h 16m 38s
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
13:06:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.146 km
Perigee altitude
773.107 km
Semi-major axis
7,152.764 km
Eccentricity
0.00021
Inclination
86.3988°
RAAN
169.1614°
Arg. of periapsis
101.4161°
True anomaly
258.70353°
Mean anomaly
258.7274°
Eccentric anomaly
258.71547°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000020911
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