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 | 8 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 8 hours ago
0 IRIDIUM 114
1 41923U 17003G 24361.23094989 .00000836 00000-0 29132-3 0 9997
2 41923 86.3969 313.2363 0002016 79.9447 280.1976 14.34217775416142Epoch: 2024-12-26T05:32Z
Definitive object data (Epoch: 2024-12-26T05:32:34.07Z)
| Latitude | -0.00004° |
| Longitude | 134.88102° |
| Altitude | 780.463 km |
| Speed | 7.464 km/s |
| True Right ascension | 20h 52m 56s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -41.13781° |
| Longitude | 131.6022° |
| Altitude | 794.234 km |
| Speed | 7.455 km/s |
| Apparent Right ascension | 22h 45m 05s |
| Apparent Declination | -45° 26' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:05:09 |
| Azimuth | 113.829° SE |
| Elevation | -63.888° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.074 km |
| Perigee altitude | 773.19 km |
| Semi-major axis | 7,152.769 km |
| Eccentricity | 0.0002016 |
| Inclination | 86.3969° |
| RAAN | 313.2363° |
| Arg. of periapsis | 79.9447° |
| True anomaly | 280.17486° |
| Mean anomaly | 280.1976° |
| Eccentric anomaly | 280.18623° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.00029132 |
| 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-26 20:44:25.982Z | 135.017° SSE | 2024-12-26 20:48:25.982Z | 74.953° E | 24.743° | 2024-12-26 20:51:25.982Z | 32.753° NE |
| 7 mins | 2024-12-26 22:25:25.982Z | 227.33° WSW | 2024-12-26 22:28:25.982Z | 275.371° WNW | 27.384° | 2024-12-26 22:32:25.982Z | 336.84° NNW |
| 8 mins | 2024-12-27 08:55:25.982Z | 7.824° NNE | 2024-12-27 08:59:25.982Z | 113.411° SE | 41.484° | 2024-12-27 09:03:25.982Z | 166.493° S |
Authenticating...
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