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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: 1 day ago

TLE from 1 day ago
0 IRIDIUM 106
1 41917U 17003A   26079.21039680  .00000077  00000-0  20404-4 0  9994
2 41917  86.3956 125.7653 0002353 105.2173 254.9283 14.34217962480455
Epoch: 2026-03-20T05:02Z
TLE epoch observation values (Epoch: 2026-03-20T05:02:58.283Z)
Latitude
-0.00004°
Longitude
-127.72628°
Altitude
781.156 km
Speed
7.463 km/s
True Right ascension
08h 23m 03s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
19:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.314 km
Perigee altitude
772.948 km
Semi-major axis
7,152.768 km
Eccentricity
0.00024
Inclination
86.3956°
RAAN
125.7653°
Arg. of periapsis
105.2173°
True anomaly
254.90227°
Mean anomaly
254.9283°
Eccentric anomaly
254.91528°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000020404
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