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 (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: 21 hours ago

TLE from 21 hours ago
0 CZ-3B R/B
1 62486U 25002B   26255.44109718  .00455049  17204-6  98103-3 0  9990
2 62486  28.4679 322.7855 4681965 177.5618 186.0072  6.38244680 16406
Epoch: 2026-09-12T10:35Z
TLE epoch observation values (Epoch: 2026-09-12T10:35:10.796Z)
Latitude
Longitude
172.5457°
Altitude
11,632.399 km
Speed
3.435 km/s
True Right ascension
21h 31m 09s
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
23:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
11,651.324 km
Perigee altitude
152.413 km
Semi-major axis
12,280.006 km
Eccentricity
0.4682
Inclination
28.4679°
RAAN
322.7855°
Arg. of periapsis
177.5618°
True anomaly
182.46381°
Mean anomaly
186.0072°
Eccentric anomaly
184.09266°
Mean motion
1.59494 °/min
Orbital period
225.71 mins
BSTAR
0.00098103
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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