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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Identifier
62486, 2025-002B
Orbit
HEO
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 (1 year ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 3.3 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CZ-3B R/B
1 62486U 25002B   26042.08635208  .00151075 -31646-6  12420-2 0  9998
2 62486  28.4046 186.8751 6076408 172.6959 203.6880  4.03618706  5645
Epoch: 2026-02-11T02:04Z
TLE epoch observation values (Epoch: 2026-02-11T02:04:20.819Z)
Latitude
-0.00001°
Longitude
14.62081°
Altitude
20,069.987 km
Speed
2.495 km/s
True Right ascension
12h 27m 27s
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
17:36:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,415.671 km
Perigee altitude
161.133 km
Semi-major axis
16,666.539 km
Eccentricity
0.60764
Inclination
28.4046°
RAAN
186.8751°
Arg. of periapsis
172.6959°
True anomaly
187.3407°
Mean anomaly
203.688°
Eccentric anomaly
194.79659°
Mean motion
1.00873 °/min
Orbital period
356.88 mins
BSTAR
0.001242
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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