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). Payloads include a variety of satellites, spacecraft, and rockets 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)
IRIDIUM 108 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 7 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Trap Box + 2 Pan, 9.4 m |
| Radar Cross Section | 14.423 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 IRIDIUM 108
1 41924U 17003H 24361.25923780 .00000471 00000-0 16100-3 0 9996
2 41924 86.3962 281.5385 0002075 88.5401 271.6032 14.34213567418008Epoch: 2024-12-26T06:13Z
Definitive object data (Epoch: 2024-12-26T06:13:18.145Z)
| Latitude | -0.0001° |
| Longitude | 92.97169° |
| Altitude | 780.691 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 46m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 55.30613° |
| Longitude | 98.04255° |
| Altitude | 785.687 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 22h 07m 08s |
| Apparent Declination | 14° 44' 00" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:32:13 |
| Azimuth | 39.446° NE |
| Elevation | -25.776° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.13 km |
| Perigee altitude | 773.161 km |
| Semi-major axis | 7,152.783 km |
| Eccentricity | 0.0002075 |
| Inclination | 86.3962° |
| RAAN | 281.5385° |
| Arg. of periapsis | 88.5401° |
| True anomaly | 271.57943° |
| Mean anomaly | 271.6032° |
| Eccentric anomaly | 271.59132° |
| Mean motion | 3.58782 °/min |
| BSTAR | 0.000161 |
| Orbital period | 100.34 mins |
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
| IRIDIUM 106, 41917 |
| IRIDIUM 103, 41918 |
| IRIDIUM 109, 41919 |
| IRIDIUM 102, 41920 |
| IRIDIUM 105, 41921 |
| IRIDIUM 104, 41922 |
| IRIDIUM 114, 41923 |
| IRIDIUM 108, 41924 |
| IRIDIUM 112, 41925 |
| IRIDIUM 111, 41926 |
IRIDIUM 108 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 19:44:35.192Z | 194.531° SSW | 2024-12-26 19:48:35.192Z | 301.492° NW | 42.049° | 2024-12-26 19:52:35.192Z | 355.357° N |
| 7 mins | 2024-12-27 06:15:35.192Z | 30.576° NE | 2024-12-27 06:18:35.192Z | 80.042° E | 26.822° | 2024-12-27 06:22:35.192Z | 138.097° SSE |
| 6 mins | 2024-12-27 07:56:35.192Z | 320.263° NNW | 2024-12-27 07:59:35.192Z | 268.833° W | 25.368° | 2024-12-27 08:02:35.192Z | 225.773° WSW |
Authenticating...
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