OBJECT E, 57428 (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 E, 57428 was a satellite owned by CNSA (CN) in LEO that was launched on Sun, 23 Jul 2023 UTC launched 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.
57428 intel report (Beta)
OBJECT E details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 8 months ago |
| Origin | |
| Manufacturer | CAST |
| Mission | Decayed spacecraft |
| Bus & Motor | Unknown |
| Mass | Unknown |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 8 months ago
0 OBJECT E
1 57428U 23104E 24121.47672315 .14555776 25151-5 63075-3 0 9994
2 57428 97.3282 196.6327 0015068 270.3772 89.5802 16.41890573 43554Definitive object data (Epoch: 2024-04-30T11:26:28.88Z)
| Latitude | 0° |
| Longitude | 166.11217° |
| Altitude | 163.977 km |
| Speed | 7.808 km/s |
| True Right ascension | 13h 06m 31s |
| True Declination | 0° 00' 00" |
| 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 | 167.428 km |
| Perigee altitude | 147.732 km |
| Semi-major axis | 6,535.717 km |
| Eccentricity | 0.0015068 |
| Inclination | 97.3282° |
| RAAN | 196.6327° |
| Arg. of periapsis | 270.3772° |
| True anomaly | 89.75286° |
| Mean anomaly | 89.5802° |
| Eccentric anomaly | 89.66653° |
| Mean motion | 4.10774 °/min |
| BSTAR | 0.00063075 |
| Orbital period | 87.64 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 E 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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