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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 108
1 41924U 17003H 25310.47340801 .00000158 00000-0 49391-4 0 9993
2 41924 86.3974 149.8737 0002095 92.3285 267.8150 14.34217471463188Epoch: 2025-11-06T11:21Z
TLE epoch observation values (Epoch: 2025-11-06T11:21:42.452Z)
Latitude
-0.00007°
Longitude
-66.48441°
Altitude
780.777 km
Speed
7.463 km/s
True Right ascension
09h 59m 29s
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
20:22:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.131 km
Perigee altitude
773.134 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3974°
RAAN
149.8737°
Arg. of periapsis
92.3285°
True anomaly
267.79101°
Mean anomaly
267.815°
Eccentric anomaly
267.80301°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000049391
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-07 01:19:58.954Z | 5.91° NNE | 2025-11-07 01:23:58.954Z | 59.43° ENE | 40.945° | 2025-11-07 01:28:58.954Z | 165.729° S |
| 4 mins | 2025-11-07 03:02:58.954Z | 301.205° NW | 2025-11-07 03:04:58.954Z | 276.136° WNW | 13.547° | 2025-11-07 03:06:58.954Z | 252.966° W |
| 8 mins | 2025-11-07 14:16:58.954Z | 200.09° SSW | 2025-11-07 14:19:58.954Z | 253.58° W | 40.425° | 2025-11-07 14:24:58.954Z | 353.724° N |
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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