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: 4 hours ago
TLE from 4 hours ago
0 IRIDIUM 106
1 41917U 17003A 26035.53530316 .00000092 00000-0 25637-4 0 9993
2 41917 86.4026 144.0014 0001847 88.5188 271.6219 14.34218194474192Epoch: 2026-02-04T12:50Z
TLE epoch observation values (Epoch: 2026-02-04T12:50:50.193Z)
Latitude
-0.00003°
Longitude
176.59177°
Altitude
780.68 km
Speed
7.464 km/s
True Right ascension
09h 36m 00s
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
19:05:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.951 km
Perigee altitude
773.309 km
Semi-major axis
7,152.767 km
Eccentricity
0.00018
Inclination
86.4026°
RAAN
144.0014°
Arg. of periapsis
88.5188°
True anomaly
271.60074°
Mean anomaly
271.6219°
Eccentric anomaly
271.61132°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000025637
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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 | 2026-02-04 18:27:26.616Z | 27.502° NE | 2026-02-04 18:31:26.616Z | 89.412° E | 24.797° | 2026-02-04 18:34:26.616Z | 131.497° SE |
| 7 mins | 2026-02-04 20:08:26.616Z | 327.4° NNW | 2026-02-04 20:11:26.616Z | 280.183° WNW | 27.264° | 2026-02-04 20:15:26.616Z | 219.689° SW |
| 8 mins | 2026-02-05 07:23:26.616Z | 163.445° S | 2026-02-05 07:27:26.616Z | 69.249° E | 40.518° | 2026-02-05 07:31:26.616Z | 11.815° NNE |
| 4 mins | 2026-02-05 09:06:26.616Z | 262.812° W | 2026-02-05 09:08:26.616Z | 288.227° WNW | 14.395° | 2026-02-05 09:10:26.616Z | 312.773° NW |
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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