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 (10 months 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: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 62486U 25002B   25302.34655662  .00254244  31771-6  66922-3 0  9998
2 62486  28.4005 263.2268 6322326  48.5494 350.6830  3.67788569  1582
Epoch: 2025-10-29T08:19Z
TLE epoch observation values (Epoch: 2025-10-29T08:19:02.491Z)
Latitude
0.00002°
Longitude
100.52119°
Altitude
1,129.231 km
Speed
9.149 km/s
True Right ascension
17h 32m 48s
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
04:05:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
22,564.524 km
Perigee altitude
143.095 km
Semi-major axis
17,731.946 km
Eccentricity
0.63223
Inclination
28.4005°
RAAN
263.2268°
Arg. of periapsis
48.5494°
True anomaly
311.53484°
Mean anomaly
350.683°
Eccentric anomaly
335.87998°
Mean motion
0.9192 °/min
Orbital period
391.65 mins
BSTAR
0.00066922
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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