IRIDIUM 124, 42810
Orbit data source: Space-Track
IRIDIUM 124, 42810 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 25 Jun 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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42810 intel report (Beta)
IRIDIUM 124 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 7 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 7 hours ago
0 IRIDIUM 124
1 42810U 17039H 24361.46106592 .00001149 00000-0 33557-3 0 9995
2 42810 86.4515 155.1608 0001983 105.9250 254.2170 14.43278108397553Epoch: 2024-12-26T11:03Z
Definitive object data (Epoch: 2024-12-26T11:03:56.095Z)
| Latitude | 0.00002° |
| Longitude | -106.26306° |
| Altitude | 751.137 km |
| Speed | 7.479 km/s |
| True Right ascension | 10h 20m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 83.35155° |
| Longitude | -74.43581° |
| Altitude | 760.049 km |
| Speed | 7.482 km/s |
| Apparent Right ascension | 06h 07m 53s |
| Apparent Declination | 32° 13' 24" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:29:04 |
| Azimuth | 351.41° N |
| Elevation | -17.303° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 746.051 km |
| Perigee altitude | 743.226 km |
| Semi-major axis | 7,122.776 km |
| Eccentricity | 0.0001983 |
| Inclination | 86.4515° |
| RAAN | 155.1608° |
| Arg. of periapsis | 105.925° |
| True anomaly | 254.19513° |
| Mean anomaly | 254.217° |
| Eccentric anomaly | 254.20607° |
| Mean motion | 3.61052 °/min |
| BSTAR | 0.00033557 |
| Orbital period | 99.71 mins |
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Other satellites on launch #39 in the year 2017 (2017-06-25 UTC)
| IRIDIUM 113, 42803 |
| IRIDIUM 123, 42804 |
| IRIDIUM 120, 42805 |
| IRIDIUM 115, 42806 |
| IRIDIUM 118, 42807 |
| IRIDIUM 117, 42808 |
| IRIDIUM 126, 42809 |
| IRIDIUM 124, 42810 |
| IRIDIUM 128, 42811 |
| IRIDIUM 121, 42812 |
IRIDIUM 124 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 | 2024-12-26 21:37:37.987Z | 29.017° NE | 2024-12-26 21:41:37.987Z | 83.19° E | 20.191° | 2024-12-26 21:44:37.987Z | 123.489° SE |
| 7 mins | 2024-12-26 23:18:37.987Z | 330.108° NNW | 2024-12-26 23:21:37.987Z | 271.132° WNW | 31.746° | 2024-12-26 23:25:37.987Z | 209.874° SW |
| 7 mins | 2024-12-27 10:29:37.987Z | 146.763° SSE | 2024-12-27 10:32:37.987Z | 89.76° E | 33.699° | 2024-12-27 10:36:37.987Z | 20.697° NNE |
| 5 mins | 2024-12-27 12:10:37.987Z | 248.555° W | 2024-12-27 12:12:37.987Z | 276.854° WNW | 18.719° | 2024-12-27 12:15:37.987Z | 319.981° NNW |
Authenticating...
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