OBJECT A, 57424
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT A, 57424 is a Chinese satellite in SSO that was launched on Sun, 23 Jul 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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57424 intel report (Beta)
OBJECT A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | DFH |
| Mission | Operational Commercial Radar Imaging |
| Bus & Motor | AS, Unknown motor |
| Mass | ~100 kg wet, ~100 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 2 Pan, 1.5 m |
| Radar Cross Section | 0.363 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 OBJECT A
1 57424U 23104A 24356.13442466 .00010072 00000-0 35672-3 0 9998
2 57424 97.3360 62.0280 0009492 251.4390 108.5819 15.29273293 78963Epoch: 2024-12-21T03:13Z
Definitive object data (Epoch: 2024-12-21T03:13:34.29Z)
| Latitude | -0.00008° |
| Longitude | -76.55481° |
| Altitude | 483.168 km |
| Speed | 7.623 km/s |
| True Right ascension | 04h 08m 06s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -3.73525° |
| Longitude | 103.38641° |
| Altitude | 479.003 km |
| Speed | 7.627 km/s |
| Apparent Right ascension | 19h 07m 27s |
| Apparent Declination | -38° 32' 47" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:28:57 |
| Azimuth | 117.067° SE |
| Elevation | -30.011° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 481.439 km |
| Perigee altitude | 468.429 km |
| Semi-major axis | 6,853.071 km |
| Eccentricity | 0.0009492 |
| Inclination | 97.336° |
| RAAN | 62.028° |
| Arg. of periapsis | 251.439° |
| True anomaly | 108.68496° |
| Mean anomaly | 108.5819° |
| Eccentric anomaly | 108.63343° |
| Mean motion | 3.82574 °/min |
| BSTAR | 0.00035672 |
| Orbital period | 94.1 mins |
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Other satellites on launch #104 in the year 2023 (2023-07-23 UTC)
| OBJECT A, 57424 |
| OBJECT B, 57425 |
| OBJECT C, 57426 |
| OBJECT D, 57427 (Decayed) |
| OBJECT E, 57428 (Decayed) |
| OBJECT F, 57429 |
OBJECT A 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 | 2024-12-21 17:55:59.275Z | 342.704° N | 2024-12-21 17:57:59.275Z | 279.691° WNW | 31.933° | 2024-12-21 18:00:59.275Z | 217.987° SW |
| 5 mins | 2024-12-22 04:29:59.275Z | 148.509° SSE | 2024-12-22 04:31:59.275Z | 56.713° ENE | 41.023° | 2024-12-22 04:34:59.275Z | 356.083° N |
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