IRIDIUM 134, 43075
Orbit data source: Space-Track
IRIDIUM 134, 43075 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 23 Dec 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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43075 intel report (Beta)
IRIDIUM 134 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 11 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 11 hours ago
0 IRIDIUM 134
1 43075U 17083F 24361.07137586 .00000067 00000-0 17017-4 0 9994
2 43075 86.3989 186.9463 0001897 92.7199 267.4214 14.34217620366970Epoch: 2024-12-26T01:42Z
Definitive object data (Epoch: 2024-12-26T01:42:46.874Z)
| Latitude | -0.00001° |
| Longitude | 66.19496° |
| Altitude | 780.78 km |
| Speed | 7.463 km/s |
| True Right ascension | 12h 27m 47s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -56.73713° |
| Longitude | -108.52275° |
| Altitude | 800.861 km |
| Speed | 7.451 km/s |
| Apparent Right ascension | 00h 29m 06s |
| Apparent Declination | -48° 44' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:13:10 |
| Azimuth | 196.537° SSW |
| Elevation | -80.733° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 775.989 km |
| Perigee altitude | 773.275 km |
| Semi-major axis | 7,152.769 km |
| Eccentricity | 0.0001897 |
| Inclination | 86.3989° |
| RAAN | 186.9463° |
| Arg. of periapsis | 92.7199° |
| True anomaly | 267.39968° |
| Mean anomaly | 267.4214° |
| Eccentric anomaly | 267.41054° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.000017017 |
| Orbital period | 100.34 mins |
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Other satellites on launch #83 in the year 2017 (2017-12-23 UTC)
| IRIDIUM 135, 43070 |
| IRIDIUM 138, 43071 |
| IRIDIUM 116, 43072 |
| IRIDIUM 130, 43073 |
| IRIDIUM 151, 43074 |
| IRIDIUM 134, 43075 |
| IRIDIUM 137, 43076 |
| IRIDIUM 141, 43077 |
| IRIDIUM 153, 43078 |
| IRIDIUM 131, 43079 |
IRIDIUM 134 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 | 2024-12-26 13:32:35.400Z | 196.739° SSW | 2024-12-26 13:37:35.400Z | 293.057° NW | 39.88° | 2024-12-26 13:41:35.400Z | 352.146° N |
| 7 mins | 2024-12-27 00:04:35.400Z | 27.283° NE | 2024-12-27 00:07:35.400Z | 79.519° E | 29.63° | 2024-12-27 00:11:35.400Z | 142.15° SSE |
| 6 mins | 2024-12-27 01:45:35.400Z | 317.725° NNW | 2024-12-27 01:48:35.400Z | 270.016° WNW | 22.754° | 2024-12-27 01:51:35.400Z | 229.619° WSW |
Authenticating...
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