IRIDIUM 112, 41925
Orbit data source: Space-Track
IRIDIUM 112, 41925 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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41925 intel report (Beta)
IRIDIUM 112 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 6 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 6 hours ago
0 IRIDIUM 112
1 41925U 17003J 24361.28803417 .00000602 00000-0 20792-3 0 9992
2 41925 86.3964 313.0790 0002409 79.4953 280.6514 14.34218414416171Epoch: 2024-12-26T06:54Z
Definitive object data (Epoch: 2024-12-26T06:54:46.152Z)
| Latitude | -0.00002° |
| Longitude | 114.11711° |
| Altitude | 780.398 km |
| Speed | 7.464 km/s |
| True Right ascension | 20h 52m 18s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -39.04375° |
| Longitude | -63.07583° |
| Altitude | 793.972 km |
| Speed | 7.455 km/s |
| Apparent Right ascension | 05h 13m 39s |
| Apparent Declination | -62° 57' 38" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:18:48 |
| Azimuth | 215.966° SW |
| Elevation | -42.014° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.353 km |
| Perigee altitude | 772.906 km |
| Semi-major axis | 7,152.766 km |
| Eccentricity | 0.0002409 |
| Inclination | 86.3964° |
| RAAN | 313.079° |
| Arg. of periapsis | 79.4953° |
| True anomaly | 280.62427° |
| Mean anomaly | 280.6514° |
| Eccentric anomaly | 280.63783° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.00020792 |
| 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 112 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-26 20:27:12.228Z | 115.99° SE | 2024-12-26 20:30:12.228Z | 75.575° E | 17.978° | 2024-12-26 20:33:12.228Z | 38.694° NE |
| 7 mins | 2024-12-26 22:07:12.228Z | 213.801° SW | 2024-12-26 22:10:12.228Z | 276.168° WNW | 35.787° | 2024-12-26 22:14:12.228Z | 345.691° N |
| 8 mins | 2024-12-27 08:37:12.228Z | 19.133° NNE | 2024-12-27 08:40:12.228Z | 68.62° E | 33.891° | 2024-12-27 08:45:12.228Z | 153.064° SSE |
| 5 mins | 2024-12-27 10:19:12.228Z | 305.994° NW | 2024-12-27 10:21:12.228Z | 276.263° WNW | 19.083° | 2024-12-27 10:24:12.228Z | 237.628° WSW |
Authenticating...
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