IRIDIUM 158, 43571
Orbit data source: Space-Track
IRIDIUM 158, 43571 is a payload satellite owned by Iridium (US) in LEO that was launched on Wed, 25 Jul 2018 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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43571 intel report (Beta)
IRIDIUM 158 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 20 hours ago |
| Origin | |
| Manufacturer | NGIS 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 20 hours ago
0 IRIDIUM 158
1 43571U 18061C 24361.06896277 .00000004 00000-0 -56339-5 0 9993
2 43571 86.3965 281.6038 0001818 77.6946 282.4453 14.34217488336231Epoch: 2024-12-26T01:39Z
Definitive object data (Epoch: 2024-12-26T01:39:18.383Z)
| Latitude | -0.00004° |
| Longitude | 161.72354° |
| Altitude | 780.439 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 46m 24s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -39.08411° |
| Longitude | 158.46038° |
| Altitude | 793.196 km |
| Speed | 7.455 km/s |
| Apparent Right ascension | 14h 30m 09s |
| Apparent Declination | -68° 59' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:57:01 |
| Azimuth | 207.328° SW |
| Elevation | -39.137° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 775.933 km |
| Perigee altitude | 773.332 km |
| Semi-major axis | 7,152.77 km |
| Eccentricity | 0.0001818 |
| Inclination | 86.3965° |
| RAAN | 281.6038° |
| Arg. of periapsis | 77.6946° |
| True anomaly | 282.42496° |
| Mean anomaly | 282.4453° |
| Eccentric anomaly | 282.43513° |
| Mean motion | 3.58783 °/min |
| BSTAR | -0.0000056339 |
| Orbital period | 100.34 mins |
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Other satellites on launch #61 in the year 2018 (2018-07-25 UTC)
| IRIDIUM 160, 43569 |
| IRIDIUM 166, 43570 |
| IRIDIUM 158, 43571 |
| IRIDIUM 165, 43572 |
| IRIDIUM 155, 43573 |
| IRIDIUM 154, 43574 |
| IRIDIUM 163, 43575 |
| IRIDIUM 156, 43576 |
| IRIDIUM 164, 43577 |
| IRIDIUM 159, 43578 |
IRIDIUM 158 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 | 2024-12-27 06:42:00.849Z | 9.285° NNE | 2024-12-27 06:46:00.849Z | 76.002° E | 39.508° | 2024-12-27 06:51:00.849Z | 162.486° S |
| 4 mins | 2024-12-27 08:25:00.849Z | 299.277° NW | 2024-12-27 08:26:00.849Z | 286.17° WNW | 15.185° | 2024-12-27 08:29:00.849Z | 248.863° W |
| 9 mins | 2024-12-27 19:38:00.849Z | 192.702° SSW | 2024-12-27 19:42:00.849Z | 263.9° W | 42.712° | 2024-12-27 19:47:00.849Z | 356.611° N |
Authenticating...
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