CZ-3B R/B, 62486

Orbit data source: Space-Track

CZ-3B R/B, 62486 is space debris 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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Identifier
62486, 2025-002B
Orbit
Active
Country
Flag of CNCN / PRC
Related business
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 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 CZ-3B R/B
1 62486U 25002B   26300.95090396  .00294501 -39909-6  65880-3 0  9995
2 62486  28.4719 253.8068 4496999 289.9982  27.9581  6.71619317 19393
Epoch: 2026-10-27T22:49Z
TLE epoch observation values (Epoch: 2026-10-27T22:49:18.102Z)
Latitude
-0.00002°
Longitude
-124.82534°
Altitude
1,829.043 km
Speed
7.972 km/s
True Right ascension
16h 55m 13s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:29:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,829.6 km
Perigee altitude
153.849 km
Semi-major axis
11,869.861 km
Eccentricity
0.4497
Inclination
28.4719°
RAAN
253.8068°
Arg. of periapsis
289.9982°
True anomaly
70.05523°
Mean anomaly
27.9581°
Eccentric anomaly
46.71421°
Mean motion
1.67832 °/min
Orbital period
214.5 mins
BSTAR
0.0006588
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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