IRIDIUM 154, 43574
Orbit data source: Space-Track
IRIDIUM 154, 43574 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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43574 intel report (Beta)
IRIDIUM 154 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 13 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 13 hours ago
0 IRIDIUM 154
1 43574U 18061F 24361.31631913 .00000796 00000-0 27704-3 0 9997
2 43574 86.3965 281.5392 0002210 83.7691 276.3757 14.34217612336315Epoch: 2024-12-26T07:35Z
Definitive object data (Epoch: 2024-12-26T07:35:29.972Z)
| Latitude | 0.00001° |
| Longitude | 72.36685° |
| Altitude | 780.543 km |
| Speed | 7.464 km/s |
| True Right ascension | 18h 46m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -67.68073° |
| Longitude | 63.36197° |
| Altitude | 804.656 km |
| Speed | 7.449 km/s |
| Apparent Right ascension | 09h 53m 01s |
| Apparent Declination | -75° 17' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:03:08 |
| Azimuth | 191.091° SSW |
| Elevation | -52.503° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.213 km |
| Perigee altitude | 773.051 km |
| Semi-major axis | 7,152.769 km |
| Eccentricity | 0.000221 |
| Inclination | 86.3965° |
| RAAN | 281.5392° |
| Arg. of periapsis | 83.7691° |
| True anomaly | 276.35053° |
| Mean anomaly | 276.3757° |
| Eccentric anomaly | 276.36312° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.00027704 |
| 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 154 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-27 05:58:16.680Z | 49.59° ENE | 2024-12-27 06:00:16.680Z | 79.638° E | 19.404° | 2024-12-27 06:03:16.680Z | 119.281° SE |
| 8 mins | 2024-12-27 07:37:16.680Z | 338.121° N | 2024-12-27 07:41:16.680Z | 265.484° W | 33.963° | 2024-12-27 07:45:16.680Z | 206.465° SW |
| 8 mins | 2024-12-27 18:53:16.680Z | 147.441° SSE | 2024-12-27 18:56:16.680Z | 92.254° ESE | 34.284° | 2024-12-27 19:01:16.680Z | 16.584° NNE |
| 5 mins | 2024-12-27 20:35:16.680Z | 252.526° W | 2024-12-27 20:37:16.680Z | 281.567° WNW | 19.227° | 2024-12-27 20:40:16.680Z | 322.54° NNW |
Authenticating...
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