IRIDIUM 108, 41924
Orbit data source: Space-Track
IRIDIUM 108, 41924 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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41924 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: 10 hours ago
TLE from 10 hours ago
0 IRIDIUM 108
1 41924U 17003H 25311.10132479 .00000114 00000-0 33488-4 0 9996
2 41924 86.3974 149.6114 0002099 92.5390 267.6047 14.34217451463279Epoch: 2025-11-07T02:25Z
TLE epoch observation values (Epoch: 2025-11-07T02:25:54.461Z)
Latitude
0.00004°
Longitude
66.58436°
Altitude
780.782 km
Speed
7.463 km/s
True Right ascension
09h 58m 26s
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
09:01:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.134 km
Perigee altitude
773.131 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3974°
RAAN
149.6114°
Arg. of periapsis
92.539°
True anomaly
267.58067°
Mean anomaly
267.6047°
Eccentric anomaly
267.59268°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000033488
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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 108 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-07 14:15:17.326Z | 194.478° SSW | 2025-11-07 14:20:17.326Z | 270.473° WNW | 40.928° | 2025-11-07 14:25:17.326Z | 354.534° N |
| 8 mins | 2025-11-08 00:47:17.326Z | 24.397° NE | 2025-11-08 00:50:17.326Z | 69.452° E | 28.506° | 2025-11-08 00:55:17.326Z | 144.621° SSE |
| 7 mins | 2025-11-08 02:28:17.326Z | 322.706° NNW | 2025-11-08 02:31:17.326Z | 277.859° WNW | 23.6° | 2025-11-08 02:35:17.326Z | 224.29° SW |
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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