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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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 IRIDIUM 106
1 41917U 17003A 25293.78946836 .00000192 00000-0 61632-4 0 9999
2 41917 86.4034 188.5510 0001872 70.6485 289.4913 14.34219145458899Epoch: 2025-10-20T18:56Z
TLE epoch observation values (Epoch: 2025-10-20T18:56:50.066Z)
Latitude
-0.00002°
Longitude
-125.14435°
Altitude
780.267 km
Speed
7.464 km/s
True Right ascension
12h 34m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:48:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.966 km
Perigee altitude
773.288 km
Semi-major axis
7,152.764 km
Eccentricity
0.00019
Inclination
86.4034°
RAAN
188.551°
Arg. of periapsis
70.6485°
True anomaly
289.47108°
Mean anomaly
289.4913°
Eccentric anomaly
289.48119°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000061632
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-21 16:49:42.774Z | 142.975° SSE | 2025-10-21 16:53:42.774Z | 92.801° ESE | 26.229° | 2025-10-21 16:57:42.774Z | 30.094° NE |
| 7 mins | 2025-10-21 18:31:42.774Z | 231.008° WSW | 2025-10-21 18:34:42.774Z | 278.666° WNW | 25.87° | 2025-10-21 18:38:42.774Z | 336.39° NNW |
| 8 mins | 2025-10-22 05:01:42.774Z | 5.954° NNE | 2025-10-22 05:04:42.774Z | 50.597° ENE | 42.45° | 2025-10-22 05:09:42.774Z | 169.647° S |
| 4 mins | 2025-10-22 16:19:42.774Z | 95.193° ESE | 2025-10-22 16:20:42.774Z | 81.623° E | 15.794° | 2025-10-22 16:23:42.774Z | 44.416° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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