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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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: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 106
1 41917U 17003A 26125.39715613 -.00000018 00000-0 -13446-4 0 9997
2 41917 86.3933 106.4470 0002418 80.0312 280.1156 14.34217280487078Epoch: 2026-05-05T09:31Z
TLE epoch observation values (Epoch: 2026-05-05T09:31:54.289Z)
Latitude
-0.00009°
Longitude
100.1982°
Altitude
780.416 km
Speed
7.464 km/s
True Right ascension
07h 05m 47s
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
23:58:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.363 km
Perigee altitude
772.904 km
Semi-major axis
7,152.77 km
Eccentricity
0.00024
Inclination
86.3933°
RAAN
106.447°
Arg. of periapsis
80.0312°
True anomaly
280.08832°
Mean anomaly
280.1156°
Eccentric anomaly
280.10196°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000013446
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-05 23:02:31.048Z | 167.911° S | 2026-05-05 23:06:31.048Z | 105.841° ESE | 41.833° | 2026-05-05 23:11:31.048Z | 9.503° NNE |
| 4 mins | 2026-05-06 00:46:31.048Z | 268.164° W | 2026-05-06 00:47:31.048Z | 280.478° WNW | 13.408° | 2026-05-06 00:50:31.048Z | 316.231° NNW |
| 4 mins | 2026-05-06 09:35:31.048Z | 57.15° ENE | 2026-05-06 09:36:31.048Z | 70.601° E | 15.782° | 2026-05-06 09:39:31.048Z | 108.75° ESE |
| 8 mins | 2026-05-06 11:14:31.048Z | 341.995° N | 2026-05-06 11:17:31.048Z | 290.231° WNW | 38.494° | 2026-05-06 11:22:31.048Z | 197.166° SSW |
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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