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: 15 hours ago
TLE from 15 hours ago
0 IRIDIUM 106
1 41917U 17003A 25354.90669306 .00000026 00000-0 23309-5 0 9991
2 41917 86.3989 163.0440 0002449 96.6047 263.5428 14.34217787467658Epoch: 2025-12-20T21:45Z
TLE epoch observation values (Epoch: 2025-12-20T21:45:38.280Z)
Latitude
0.00002°
Longitude
106.90773°
Altitude
780.916 km
Speed
7.463 km/s
True Right ascension
10h 52m 10s
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
11:48:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.383 km
Perigee altitude
772.88 km
Semi-major axis
7,152.768 km
Eccentricity
0.00024
Inclination
86.3989°
RAAN
163.044°
Arg. of periapsis
96.6047°
True anomaly
263.51492°
Mean anomaly
263.5428°
Eccentric anomaly
263.52886°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000023309
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
Did you know?
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 | 2025-12-21 12:57:08.916Z | 226.919° WSW | 2025-12-21 13:01:08.916Z | 278.005° WNW | 22.731° | 2025-12-21 13:05:08.916Z | 333.119° NNW |
| 8 mins | 2025-12-21 23:28:08.916Z | 0.585° NNE | 2025-12-21 23:32:08.916Z | 154.442° SSE | 43.662° | 2025-12-21 23:36:08.916Z | 175.712° S |
| 6 mins | 2025-12-22 10:44:08.916Z | 120.802° SE | 2025-12-22 10:47:08.916Z | 82.616° E | 18.348° | 2025-12-22 10:50:08.916Z | 42.671° NE |
| 8 mins | 2025-12-22 12:24:08.916Z | 211.16° SW | 2025-12-22 12:27:08.916Z | 260.547° W | 34.791° | 2025-12-22 12:32:08.916Z | 347.881° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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