IRIDIUM 105, 41921
Orbit data source: Space-Track
IRIDIUM 105, 41921 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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41921 intel report (Beta)
IRIDIUM 105 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 105
1 41921U 17003E 24361.25243490 .00000856 00000-0 29848-3 0 9996
2 41921 86.3968 281.6291 0002056 84.0094 276.1336 14.34221035418035Epoch: 2024-12-26T06:03Z
Definitive object data (Epoch: 2024-12-26T06:03:30.375Z)
| Latitude | -0.00002° |
| Longitude | 95.51804° |
| Altitude | 780.55 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 46m 30s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 42.51428° |
| Longitude | 98.68991° |
| Altitude | 782.879 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 21h 31m 42s |
| Apparent Declination | 5° 27' 22" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:18:48 |
| Azimuth | 50.364° ENE |
| Elevation | -30.558° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.091 km |
| Perigee altitude | 773.15 km |
| Semi-major axis | 7,152.758 km |
| Eccentricity | 0.0002056 |
| Inclination | 86.3968° |
| RAAN | 281.6291° |
| Arg. of periapsis | 84.0094° |
| True anomaly | 276.11017° |
| Mean anomaly | 276.1336° |
| Eccentric anomaly | 276.12189° |
| Mean motion | 3.58784 °/min |
| BSTAR | 0.00029848 |
| 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 105 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2024-12-26 19:33:12.305Z | 183.425° SSW | 2024-12-26 19:38:12.305Z | 229.637° WSW | 44.706° | 2024-12-26 19:43:12.305Z | 0.923° NNE |
| 6 mins | 2024-12-27 06:06:12.305Z | 39.805° NE | 2024-12-27 06:08:12.305Z | 69.769° E | 22.283° | 2024-12-27 06:12:12.305Z | 127.583° SE |
| 7 mins | 2024-12-27 07:46:12.305Z | 330.704° NNW | 2024-12-27 07:49:12.305Z | 281.517° WNW | 30.067° | 2024-12-27 07:53:12.305Z | 215.624° SW |
Authenticating...
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