IRIDIUM 111, 41926
Orbit data source: Space-Track
IRIDIUM 111, 41926 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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41926 intel report (Beta)
IRIDIUM 111 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 111
1 41926U 17003K 24361.27534849 .00000121 00000-0 36114-4 0 9994
2 41926 86.3966 313.1431 0002111 83.3329 276.8107 14.34217379416150Epoch: 2024-12-26T06:36Z
Definitive object data (Epoch: 2024-12-26T06:36:30.109Z)
| Latitude | -0.00003° |
| Longitude | 118.76056° |
| Altitude | 780.54 km |
| Speed | 7.464 km/s |
| True Right ascension | 20h 52m 34s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 56.70391° |
| Longitude | 124.11214° |
| Altitude | 785.882 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 23h 17m 58s |
| Apparent Declination | 13° 35' 11" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:55:52 |
| Azimuth | 28.304° NE |
| Elevation | -31.856° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.143 km |
| Perigee altitude | 773.123 km |
| Semi-major axis | 7,152.77 km |
| Eccentricity | 0.0002111 |
| Inclination | 86.3966° |
| RAAN | 313.1431° |
| Arg. of periapsis | 83.3329° |
| True anomaly | 276.78668° |
| Mean anomaly | 276.8107° |
| Eccentric anomaly | 276.79869° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.000036114 |
| 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 111 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 21:48:10.615Z | 192.122° SSW | 2024-12-26 21:52:10.615Z | 301.051° NW | 42.91° | 2024-12-26 21:56:10.615Z | 356.39° N |
| 7 mins | 2024-12-27 08:19:10.615Z | 30.989° NE | 2024-12-27 08:22:10.615Z | 78.618° E | 25.816° | 2024-12-27 08:26:10.615Z | 136.159° SSE |
| 7 mins | 2024-12-27 10:00:10.615Z | 322.085° NNW | 2024-12-27 10:03:10.615Z | 269.931° W | 26.452° | 2024-12-27 10:07:10.615Z | 217.693° SW |
Authenticating...
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