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, 3.3 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 62486U 25002B   26209.38089075  .00766398  78433-6  13160-2 0  9997
2 62486  28.4805  26.0623 4978798  74.4433 333.6354  5.86152837 13579
Epoch: 2026-07-28T09:08Z
TLE epoch observation values (Epoch: 2026-07-28T09:08:28.960Z)
Latitude
-0.00004°
Longitude
-57.1033°
Altitude
2,236.592 km
Speed
7.866 km/s
True Right ascension
01h 44m 16s
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
10:59:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,089.785 km
Perigee altitude
147.912 km
Semi-major axis
12,996.986 km
Eccentricity
0.49788
Inclination
28.4805°
RAAN
26.0623°
Arg. of periapsis
74.4433°
True anomaly
285.73651°
Mean anomaly
333.6354°
Eccentric anomaly
312.65611°
Mean motion
1.4648 °/min
Orbital period
245.77 mins
BSTAR
0.001316
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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