CZ-3B R/B, 60328

Orbit data source: Space-Track

CZ-3B R/B, 60328 is space debris in HEO originally from a launch on Thu, 01 Aug 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-3B R/B details

Identifier	60328, 2024-135B
Orbit	HEO
Last TLE update	2 months ago
Origin	CASC (CN / PRC)
Manufacturer	CALT
Mission	Spacecraft
Bus & Motor	CZ-3A STAGE 3, Unknown motor
Mass	~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)	2024-08-01 (5 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 2 months ago

0 CZ-3B R/B
1 60328U 24135B   24318.52791732  .00064576 -49806-6  63802-3 0  9992
2 60328  26.8897 101.8473 7051197 253.1331  24.2081  2.63467322  2625

Epoch: 2024-11-13T12:40Z

Definitive object data (Epoch: 2024-11-13T12:40:12.056Z)

Latitude	-0°
Longitude	-141.43604°
Altitude	7,607.875 km
Speed	6.245 km/s
True Right ascension	06h 46m 56s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-13.6268°
Longitude	37.94498°
Altitude	4,653.643 km
Speed	7.341 km/s
Apparent Right ascension	19h 01m 37s
Apparent Declination	-23° 13' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	07:39:19
Azimuth	28.305° NE
Elevation	-71.501°
Doppler factor	1

Orbital elements

Apogee altitude	31,386.181 km
Perigee altitude	152.756 km
Semi-major axis	22,147.605 km
Eccentricity	0.7051197
Inclination	26.8897°
RAAN	101.8473°
Arg. of periapsis	253.1331°
True anomaly	107.08174°
Mean anomaly	24.2081°
Eccentric anomaly	58.74506°
Mean motion	0.6585 °/min
BSTAR	0.00063802
Orbital period	546.7 mins