IRIDIUM 137, 43076
Orbit data source: Space-Track
IRIDIUM 137, 43076 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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43076 intel report (Beta)
IRIDIUM 137 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 13 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 13 hours ago
0 IRIDIUM 137
1 43076U 17083G 24361.01429525 .00000060 00000-0 14222-4 0 9994
2 43076 86.3991 187.0520 0002311 102.0886 258.0569 14.34217774367037Epoch: 2024-12-26T00:20Z
Definitive object data (Epoch: 2024-12-26T00:20:35.109Z)
| Latitude | -0.00002° |
| Longitude | 86.90594° |
| Altitude | 781.061 km |
| Speed | 7.463 km/s |
| True Right ascension | 12h 28m 12s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -57.4302° |
| Longitude | 81.05384° |
| Altitude | 801.524 km |
| Speed | 7.451 km/s |
| Apparent Right ascension | 03h 08m 12s |
| Apparent Declination | -82° 27' 43" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:49:56 |
| Azimuth | 186.147° SSW |
| Elevation | -45.97° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.285 km |
| Perigee altitude | 772.979 km |
| Semi-major axis | 7,152.769 km |
| Eccentricity | 0.0002311 |
| Inclination | 86.3991° |
| RAAN | 187.052° |
| Arg. of periapsis | 102.0886° |
| True anomaly | 258.03099° |
| Mean anomaly | 258.0569° |
| Eccentric anomaly | 258.04395° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.000014222 |
| 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 137 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 13:51:16.008Z | 211.63° SW | 2024-12-26 13:55:16.008Z | 267.918° W | 31.71° | 2024-12-26 14:00:16.008Z | 345.603° N |
| 8 mins | 2024-12-27 00:22:16.008Z | 12.76° NNE | 2024-12-27 00:26:16.008Z | 93.405° ESE | 38° | 2024-12-27 00:30:16.008Z | 157.778° S |
| 5 mins | 2024-12-27 02:04:16.008Z | 307.45° NW | 2024-12-27 02:06:16.008Z | 280.969° WNW | 16.341° | 2024-12-27 02:09:16.008Z | 243.923° WSW |
| 8 mins | 2024-12-27 13:18:16.008Z | 190.624° SSW | 2024-12-27 13:22:16.008Z | 299.364° NW | 43.418° | 2024-12-27 13:26:16.008Z | 357.02° N |
Authenticating...
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