CZ-3B R/B, 62486

Orbit data source: Space-Track

CZ-3B R/B, 62486 is space debris in HEO originally from a launch on Mon, 06 Jan 2025 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	62486, 2025-002B
Orbit	HEO
Last TLE update	21 hours 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)	2025-01-06 (3 weeks 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 21 hours ago

0 CZ-3B R/B
1 62486U 25002B   25024.98581018  .00032700  31102-6  60087-3 0  9997
2 62486  28.5343  37.3580 7356523 190.1557 136.2558  2.23413149   412

Epoch: 2025-01-24T23:39Z

Definitive object data (Epoch: 2025-01-24T23:39:33.999Z)

Latitude	-0.00013°
Longitude	-82.0682°
Altitude	34,707.503 km
Speed	1.81 km/s
True Right ascension	02h 29m 27s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-2.92027°
Longitude	-87.76113°
Altitude	31,957.503 km
Speed	2.16 km/s
Apparent Right ascension	02h 34m 44s
Apparent Declination	-9° 21' 33"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	21:44:16
Azimuth	108.436° ESE
Elevation	6.994°
Doppler factor	1

Orbital elements

Apogee altitude	36,528.579 km
Perigee altitude	156.75 km
Semi-major axis	24,720.802 km
Eccentricity	0.7356523
Inclination	28.5343°
RAAN	37.358°
Arg. of periapsis	190.1557°
True anomaly	169.88287°
Mean anomaly	136.2558°
Eccentric anomaly	154.44095°
Mean motion	0.55841 °/min
BSTAR	0.00060087
Orbital period	644.69 mins