IRIDIUM 165, 43572
Orbit data source: Space-Track
IRIDIUM 165, 43572 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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43572 intel report (Beta)
IRIDIUM 165 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 9 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 9 hours ago
0 IRIDIUM 165
1 43572U 18061D 24361.51294549 -.00000113 00000-0 -47257-4 0 9998
2 43572 86.3966 281.4543 0002130 84.4986 275.6452 14.34216834336327Epoch: 2024-12-26T12:18Z
Definitive object data (Epoch: 2024-12-26T12:18:38.49Z)
| Latitude | -0.00009° |
| Longitude | 1.30265° |
| Altitude | 780.572 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 45m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 48.98302° |
| Longitude | 5.28262° |
| Altitude | 784.226 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 13h 12m 34s |
| Apparent Declination | 39° 26' 54" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:17:31 |
| Azimuth | 310.171° NW |
| Elevation | 14.01° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.158 km |
| Perigee altitude | 773.111 km |
| Semi-major axis | 7,152.772 km |
| Eccentricity | 0.000213 |
| Inclination | 86.3966° |
| RAAN | 281.4543° |
| Arg. of periapsis | 84.4986° |
| True anomaly | 275.62091° |
| Mean anomaly | 275.6452° |
| Eccentric anomaly | 275.63305° |
| Mean motion | 3.58783 °/min |
| BSTAR | -0.000047257 |
| 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 165 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-27 07:19:37.073Z | 346.281° N | 2024-12-27 07:22:37.073Z | 283.722° WNW | 42.046° | 2024-12-27 07:27:37.073Z | 190.636° SSW |
| 7 mins | 2024-12-27 18:35:37.073Z | 127.95° SE | 2024-12-27 18:38:37.073Z | 76.574° E | 25.691° | 2024-12-27 18:42:37.073Z | 25.527° NE |
| 7 mins | 2024-12-27 20:15:37.073Z | 227.844° WSW | 2024-12-27 20:18:37.073Z | 273.522° WNW | 26.407° | 2024-12-27 20:22:37.073Z | 335.256° NNW |
Authenticating...
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