DECAYED

CZ-4B R/B, 60951 (Decayed)

Orbit data source: Space-Track

CZ-4B R/B, 60951 was space debris in LEO originally from a launch on Tue, 03 Sep 2024 UTC launched from the Xichang Space Center, China (XSC). 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
Identifier
60951, 2024-156G
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)
2024-09-03 (8 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.932 m
Radar Cross Section
14.536 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago
0 CZ-4B R/B
1 60951U 24156G   25068.62579449  .10191814  14649-5  77744-3 0  9992
2 60951  34.9765 158.7920 0008383 359.5098 138.6642 16.39154785 29426
Epoch: 2025-03-09T15:01Z
Definitive object data (Epoch: 2025-03-09T15:01:08.643Z)
Latitude
22.54089°
Longitude
-90.19561°
Altitude
170.806 km
Speed
7.806 km/s
True Right ascension
20h 10m 34s
True Declination
22° 24' 31"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
176.959 km
Perigee altitude
165.978 km
Semi-major axis
6,549.606 km
Eccentricity
0.0008383
Inclination
34.9765°
RAAN
158.792°
Arg. of periapsis
359.5098°
True anomaly
138.7276°
Mean anomaly
138.6642°
Eccentric anomaly
138.6959°
Mean motion
4.09468 °/min
BSTAR
0.00077744
Orbital period
87.92 mins
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CZ-4B R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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