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 25286.61257313 .00000215 00000-0 69698-4 0 9992
2 41924 86.4010 159.8365 0001969 84.7266 275.4155 14.34216608459761Epoch: 2025-10-13T14:42Z
TLE epoch observation values (Epoch: 2025-10-13T14:42:06.318Z)
Latitude
0.00003°
Longitude
-83.10267°
Altitude
780.589 km
Speed
7.464 km/s
True Right ascension
10h 39m 20s
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
22:03:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.044 km
Perigee altitude
773.227 km
Semi-major axis
7,152.772 km
Eccentricity
0.0002
Inclination
86.401°
RAAN
159.8365°
Arg. of periapsis
84.7266°
True anomaly
275.39304°
Mean anomaly
275.4155°
Eccentric anomaly
275.40427°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000069698
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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 | 2025-10-14 04:40:24.124Z | 334.959° NNW | 2025-10-14 04:44:24.124Z | 283.846° WNW | 26.152° | 2025-10-14 04:48:24.124Z | 222.421° SW |
| 8 mins | 2025-10-14 15:56:24.124Z | 166.083° S | 2025-10-14 16:00:24.124Z | 77.869° E | 41.688° | 2025-10-14 16:04:24.124Z | 11.156° NNE |
| 5 mins | 2025-10-15 02:28:24.124Z | 50.18° ENE | 2025-10-15 02:30:24.124Z | 76.396° E | 15.598° | 2025-10-15 02:33:24.124Z | 112.473° ESE |
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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