CZ-4B R/B, 61938

Orbit data source: Space-Track

CZ-4B R/B, 61938 is space debris in SSO originally from a launch on Wed, 13 Nov 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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CZ-4B R/B details

Identifier	61938, 2024-208C
Orbit	SSO
Last TLE update	15 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)	2024-11-13 (1 week ago)
Launch vehicle	Unknown
Launch site	Taiyaun Space Center, China (TSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 CZ-4B R/B
1 61938U 24208C   24325.66367889  .00017119  00000-0  67074-3 0  9998
2 61938  98.0005 330.6155 0161449 349.0153  10.7566 15.14545619  1023

Epoch: 2024-11-20T15:55Z

Definitive object data (Epoch: 2024-11-20T15:55:41.856Z)

Latitude	-0.00005°
Longitude	31.53457°
Altitude	416.015 km
Speed	7.722 km/s
True Right ascension	22h 02m 27s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	44.0735°
Longitude	-140.03582°
Altitude	623.513 km
Speed	7.499 km/s
Apparent Right ascension	13h 10m 32s
Apparent Declination	5° 45' 50"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	03:50:07
Azimuth	48.39° ENE
Elevation	-31.399°
Doppler factor	1

Orbital elements

Apogee altitude	630.716 km
Perigee altitude	407.997 km
Semi-major axis	6,897.494 km
Eccentricity	0.0161449
Inclination	98.0005°
RAAN	330.6155°
Arg. of periapsis	349.0153°
True anomaly	11.10887°
Mean anomaly	10.7566°
Eccentric anomaly	10.93203°
Mean motion	3.78884 °/min
BSTAR	0.00067074
Orbital period	95.02 mins