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 (8 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 months ago

TLE from 3 months ago
0 CZ-3B R/B
1 62486U 25002B   25139.05711270  .00363423 -24326-6  11688-2 0  9999
2 62486  28.7086 354.5539 7172030 259.9420  19.3288  2.48364471  3041
Epoch: 2025-05-19T01:22Z
TLE epoch observation values (Epoch: 2025-05-19T01:22:14.537Z)
Latitude
-0.00018°
Longitude
97.02772°
Altitude
6,401.716 km
Speed
6.713 km/s
True Right ascension
23h 38m 15s
True Declination
0° 00' 01"
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
16:53:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,179.812 km
Perigee altitude
136.451 km
Semi-major axis
23,036.268 km
Eccentricity
0.7172
Inclination
28.7086°
RAAN
354.5539°
Arg. of periapsis
259.942°
True anomaly
99.82295°
Mean anomaly
19.3288°
Eccentric anomaly
51.47883°
Mean motion
0.62076 °/min
Orbital period
579.93 mins
BSTAR
0.0011688
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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