IRIDIUM 164, 43577
Orbit data source: Space-Track
IRIDIUM 164, 43577 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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43577 intel report (Beta)
IRIDIUM 164 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 8 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 8 hours ago
0 IRIDIUM 164
1 43577U 18061J 24361.53197267 .00000503 00000-0 17248-3 0 9991
2 43577 86.3962 281.4197 0002330 89.2202 270.9261 14.34217721336354Epoch: 2024-12-26T12:46Z
Definitive object data (Epoch: 2024-12-26T12:46:02.438Z)
| Latitude | -0.00001° |
| Longitude | -5.60048° |
| Altitude | 780.692 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 45m 40s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 9.70347° |
| Longitude | -5.13331° |
| Altitude | 779.641 km |
| Speed | 7.465 km/s |
| Apparent Right ascension | 16h 10m 08s |
| Apparent Declination | -39° 40' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:34:01 |
| Azimuth | 225.499° WSW |
| Elevation | -9.749° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.298 km |
| Perigee altitude | 772.965 km |
| Semi-major axis | 7,152.769 km |
| Eccentricity | 0.000233 |
| Inclination | 86.3962° |
| RAAN | 281.4197° |
| Arg. of periapsis | 89.2202° |
| True anomaly | 270.8994° |
| Mean anomaly | 270.9261° |
| Eccentric anomaly | 270.91275° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.00017248 |
| 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 164 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 | 2024-12-27 06:06:04.213Z | 31.081° NE | 2024-12-27 06:09:04.213Z | 73.148° E | 22.857° | 2024-12-27 06:13:04.213Z | 129.773° SE |
| 7 mins | 2024-12-27 07:47:04.213Z | 328.505° NNW | 2024-12-27 07:50:04.213Z | 276.533° WNW | 29.692° | 2024-12-27 07:54:04.213Z | 215.093° SW |
| 8 mins | 2024-12-27 19:02:04.213Z | 157.938° S | 2024-12-27 19:06:04.213Z | 66.44° ENE | 37.944° | 2024-12-27 19:10:04.213Z | 13.861° NNE |
| 4 mins | 2024-12-27 20:45:04.213Z | 263.435° W | 2024-12-27 20:47:04.213Z | 290.755° WNW | 15.925° | 2024-12-27 20:49:04.213Z | 315.894° NNW |
Authenticating...
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