OBJECT B, 60250 (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 B, 60250 was a satellite owned by CNSA (CN) in LEO that was launched on Fri, 19 Jul 2024 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.
60250 intel report (Beta)
OBJECT B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | SAST |
| Mission | Decayed spacecraft |
| Bus & Motor | CZ-4 STAGE 3, Unknown motor |
| Mass | ~1,000 kg wet, ~1,000 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 2 months ago
0 OBJECT B
1 60250U 24130B 24235.98486666 .12432784 26111-5 26985-3 0 9992
2 60250 97.3929 308.5878 0019573 40.1387 46.3473 16.44862158 5536Definitive object data (Epoch: 2024-08-22T23:38:12.479Z)
| Latitude | 81.93115° |
| Longitude | -83.23061° |
| Altitude | 157.598 km |
| Speed | 7.824 km/s |
| True Right ascension | 16h 12m 20s |
| True Declination | 81° 52' 44" |
| Sunlit | Object was in daylight 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 | 162.478 km |
| Perigee | 136.924 km |
| Semi-major axis | 6,527.838 km |
| Eccentricity | 0.0019573 |
| Inclination | 97.3929° |
| RAAN | 308.5878° |
| Arg. of periapsis | 40.1387° |
| True anomaly | 46.50986° |
| Mean anomaly | 46.3473° |
| Eccentric anomaly | 46.42855° |
| Mean motion | 4.11518 °/min |
| BSTAR | 0.00026985 |
| Period | 87.48 mins |
Other satellites on launch #130 in the year 2024 (2024-07-19 UTC)
| OBJECT A, 60249 |
| OBJECT B, 60250 (Decayed) |
OBJECT B 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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