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, 4.7 m
Radar Cross Section
14.423 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 25256.82141814 .00000152 00000-0 47291-4 0 9995
2 41924 86.4042 172.2626 0002295 78.9577 281.1877 14.34217113455491Epoch: 2025-09-13T19:42Z
TLE epoch observation values (Epoch: 2025-09-13T19:42:50.527Z)
Latitude
0°
Longitude
-116.49721°
Altitude
780.402 km
Speed
7.464 km/s
True Right ascension
11h 29m 03s
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
22:26:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.275 km
Perigee altitude
772.992 km
Semi-major axis
7,152.771 km
Eccentricity
0.00023
Inclination
86.4042°
RAAN
172.2626°
Arg. of periapsis
78.9577°
True anomaly
281.1619°
Mean anomaly
281.1877°
Eccentric anomaly
281.1748°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000047291
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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 | 2025-09-14 06:19:48.416Z | 5.718° NNE | 2025-09-14 06:24:48.416Z | 96.926° ESE | 40.877° | 2025-09-14 06:28:48.416Z | 163.301° S |
| 8 mins | 2025-09-14 19:16:48.416Z | 196.957° SSW | 2025-09-14 19:20:48.416Z | 290.233° WNW | 41.327° | 2025-09-14 19:24:48.416Z | 353.451° N |
| 5 mins | 2025-09-15 05:47:48.416Z | 27.996° NE | 2025-09-15 05:50:48.416Z | 77.226° E | 28.118° | 2025-09-15 05:52:48.416Z | 118.025° SE |
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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