OBJECT D, 57427 (Decayed)
Orbit data source: Space-Track
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT D, 57427 was a satellite owned by CNSA (CN) in LEO 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. This object's orbit decayed before it could be identified.
57427 intel report (Beta)
OBJECT D details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 3 months ago |
| Origin | |
| Manufacturer | CAST |
| Mission | Decayed Commercial Communications |
| Bus & Motor | Unknown |
| Mass | Unknown |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box + 1 Pan, 10 m |
| Radar Cross Section | 16.383 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 3 months ago
0 OBJECT D
1 57427U 23104D 24276.29366333 .28605412 25133-5 66733-3 0 9996
2 57427 97.3105 352.1805 0010855 272.1620 133.6895 16.45580245 67362Definitive object data (Epoch: 2024-10-02T07:02:52.511Z)
| Latitude | 45.56696° |
| Longitude | -132.50879° |
| Altitude | 162.991 km |
| Speed | 7.81 km/s |
| True Right ascension | 22h 58m 49s |
| True Declination | 45° 22' 46" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 154.88 km |
| Perigee altitude | 140.713 km |
| Semi-major axis | 6,525.934 km |
| Eccentricity | 0.0010855 |
| Inclination | 97.3105° |
| RAAN | 352.1805° |
| Arg. of periapsis | 272.162° |
| True anomaly | 133.77936° |
| Mean anomaly | 133.6895° |
| Eccentric anomaly | 133.73444° |
| Mean motion | 4.11698 °/min |
| BSTAR | 0.00066733 |
| Orbital period | 87.44 mins |
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 D 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. |
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