CZ-4B R/B, 60250 (Decayed)
Orbit data source: Space-Track
CZ-4B R/B, 60250 was space debris in LEO originally from a launch on Fri, 19 Jul 2024 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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60250 intel report (Beta)
CZ-4B R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 6 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 | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 6 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 5536
Epoch: 2024-08-22T23:38Z
Definitive 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 altitude | 162.478 km |
Perigee altitude | 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 |
Orbital period | 87.48 mins |
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Other satellites on launch #130 in the year 2024 (2024-07-19 UTC)
GAOFEN 11-05, 60249 |
CZ-4B R/B, 60250 (Decayed) |
CZ-4B R/B Visibility forecast
Observer location: undefined°, undefined
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