DECAYED

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.

Not visible in the next 10 days
CZ-4B R/B details
Identifier
60250, 2024-130B
Orbit
Decayed
Last TLE update6 months ago
Origin
Flag of CNCNSA (CN / PRC)
ManufacturerSAST
MissionDecayed spacecraft
Bus & MotorCZ-4 STAGE 3, Unknown motor
Mass~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2024-07-19 (7 months ago)
Launch vehicleUnknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBRUnknown
Radar Cross SectionLarge (>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)
Latitude81.93115°
Longitude-83.23061°
Altitude157.598 km
Speed7.824 km/s
True Right ascension16h 12m 20s
True Declination81° 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 altitude162.478 km
Perigee altitude136.924 km
Semi-major axis6,527.838 km
Eccentricity0.0019573
Inclination97.3929°
RAAN308.5878°
Arg. of periapsis40.1387°
True anomaly46.50986°
Mean anomaly46.3473°
Eccentric anomaly46.42855°
Mean motion4.11518 °/min
BSTAR0.00026985
Orbital period87.48 mins
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Other satellites on launch #130 in the year 2024 (2024-07-19 UTC)

CZ-4B R/B Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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