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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 106
1 41917U 17003A 25256.95169413 .00000164 00000-0 51483-4 0 9997
2 41917 86.4016 203.9156 0002699 83.5911 276.5592 14.34218273453618Epoch: 2025-09-13T22:50Z
TLE epoch observation values (Epoch: 2025-09-13T22:50:26.372Z)
Latitude
-0.00005°
Longitude
-131.87197°
Altitude
780.496 km
Speed
7.464 km/s
True Right ascension
13h 35m 39s
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
22:26:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.56 km
Perigee altitude
772.699 km
Semi-major axis
7,152.767 km
Eccentricity
0.00027
Inclination
86.4016°
RAAN
203.9156°
Arg. of periapsis
83.5911°
True anomaly
276.52847°
Mean anomaly
276.5592°
Eccentric anomaly
276.54384°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000051483
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-14 07:47:47.921Z | 27.885° NE | 2025-09-14 07:51:47.921Z | 85.528° E | 23.125° | 2025-09-14 07:54:47.921Z | 127.381° SE |
| 8 mins | 2025-09-14 09:28:47.921Z | 330.946° NNW | 2025-09-14 09:31:47.921Z | 284.739° WNW | 29.064° | 2025-09-14 09:36:47.921Z | 211.867° SW |
| 8 mins | 2025-09-14 20:43:47.921Z | 160.225° S | 2025-09-14 20:47:47.921Z | 80.533° E | 39.009° | 2025-09-14 20:51:47.921Z | 14.606° NNE |
| 5 mins | 2025-09-14 22:26:47.921Z | 259.574° W | 2025-09-14 22:28:47.921Z | 285.992° WNW | 15.79° | 2025-09-14 22:31:47.921Z | 322.284° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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