IRIDIUM 114, 41923
Orbit data source: Space-Track
IRIDIUM 114, 41923 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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41923 intel report (Beta)
IRIDIUM 114 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 16 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 16 hours ago
0 IRIDIUM 114
1 41923U 17003G 24339.46317523 .00000288 00000-0 95916-4 0 9994
2 41923 86.3950 322.3399 0002304 81.2951 278.8506 14.34217401413021Epoch: 2024-12-04T11:06Z
Definitive object data (Epoch: 2024-12-04T11:06:58.339Z)
| Latitude | -0.00002° |
| Longitude | 81.83885° |
| Altitude | 780.466 km |
| Speed | 7.464 km/s |
| True Right ascension | 21h 29m 21s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -49.52601° |
| Longitude | -94.23059° |
| Altitude | 798.395 km |
| Speed | 7.452 km/s |
| Apparent Right ascension | 11h 31m 25s |
| Apparent Declination | -47° 51' 12" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 01:12:21 |
| Azimuth | 122.061° SE |
| Elevation | -70.272° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.281 km |
| Perigee altitude | 772.985 km |
| Semi-major axis | 7,152.77 km |
| Eccentricity | 0.0002304 |
| Inclination | 86.395° |
| RAAN | 322.3399° |
| Arg. of periapsis | 81.2951° |
| True anomaly | 278.82451° |
| Mean anomaly | 278.8506° |
| Eccentric anomaly | 278.83756° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.000095916 |
| 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 114 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2024-12-05 11:08:08.959Z | 0.001° NNE | 2024-12-05 11:12:08.959Z | 31.347° NE | 44.102° | 2024-12-05 11:17:08.959Z | 175.348° S |
| 5 mins | 2024-12-05 22:26:08.959Z | 108.643° ESE | 2024-12-05 22:28:08.959Z | 80.526° E | 18.152° | 2024-12-05 22:31:08.959Z | 41.56° NE |
| 8 mins | 2024-12-06 00:05:08.959Z | 211.578° SW | 2024-12-06 00:08:08.959Z | 264.774° W | 35.356° | 2024-12-06 00:13:08.959Z | 348.723° N |
Authenticating...
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