CZ-4B R/B, 60951

Orbit data source: Space-Track

CZ-4B R/B, 60951 is 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.

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CZ-4B R/B details

Identifier	60951, 2024-156G
Orbit	LEO
Last TLE update	14 hours ago
Origin	CNSA (CN / PRC)
Manufacturer	SAST
Mission	Spacecraft
Bus & Motor	CZ-4 STAGE 3, Unknown motor
Mass	~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)	2024-09-03 (4 months ago)
Launch vehicle	Unknown
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 14 hours ago

0 CZ-4B R/B
1 60951U 24156G   25014.60941920  .00150352  00000-0  92911-3 0  9993
2 60951  34.9926 174.5613 0046371 184.0196 176.0167 15.74121174 20837

Epoch: 2025-01-14T14:37Z

Definitive object data (Epoch: 2025-01-14T14:37:33.818Z)

Latitude	-0°
Longitude	-159.14327°
Altitude	377.119 km
Speed	7.668 km/s
True Right ascension	11h 38m 14s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	35.11334°
Longitude	-70.38034°
Altitude	351.127 km
Speed	7.702 km/s
Apparent Right ascension	17h 27m 59s
Apparent Declination	-1° 12' 54"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	05:22:02
Azimuth	357.619° N
Elevation	-51.275°
Doppler factor	1

Orbital elements

Apogee altitude	381.658 km
Perigee altitude	319.256 km
Semi-major axis	6,728.594 km
Eccentricity	0.0046371
Inclination	34.9926°
RAAN	174.5613°
Arg. of periapsis	184.0196°
True anomaly	176.0534°
Mean anomaly	176.0167°
Eccentric anomaly	176.03507°
Mean motion	3.93239 °/min
BSTAR	0.00092911
Orbital period	91.55 mins