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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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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 108
1 41924U 17003H 26318.38613995 .00000002 00000-0 -63675-5 0 9990
2 41924 86.3976 353.9757 0002036 92.1048 268.0381 14.34217406516636Epoch: 2026-11-14T09:16Z
TLE epoch observation values (Epoch: 2026-11-14T09:16:02.491Z)
Latitude
-0.00003°
Longitude
161.47365°
Altitude
780.769 km
Speed
7.463 km/s
True Right ascension
23h 35m 54s
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
14:56:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.089 km
Perigee altitude
773.176 km
Semi-major axis
7,152.77 km
Eccentricity
0.0002
Inclination
86.3976°
RAAN
353.9757°
Arg. of periapsis
92.1048°
True anomaly
268.01478°
Mean anomaly
268.0381°
Eccentric anomaly
268.02644°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000063675
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-15 02:07:52.995Z | 135.143° SSE | 2026-11-15 02:11:52.995Z | 84.055° E | 24.827° | 2026-11-15 02:15:52.995Z | 30.744° NE |
| 8 mins | 2026-11-15 03:48:52.995Z | 219.674° SW | 2026-11-15 03:52:52.995Z | 288.564° WNW | 34.833° | 2026-11-15 03:56:52.995Z | 342.624° N |
| 9 mins | 2026-11-15 14:18:52.995Z | 9.215° NNE | 2026-11-15 14:22:52.995Z | 81.211° E | 57.209° | 2026-11-15 14:27:52.995Z | 163.512° S |
| 4 mins | 2026-11-15 16:01:52.995Z | 297.714° NW | 2026-11-15 16:02:52.995Z | 284.632° WNW | 15.558° | 2026-11-15 16:05:52.995Z | 248.175° W |
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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