CZ-3B R/B, 62486

Orbit data source: Space-Track

CZ-3B R/B, 62486 is space debris 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
Active
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: 14 hours ago

TLE from 14 hours ago
0 CZ-3B R/B
1 62486U 25002B   26312.05625899  .00383863 -35285-6  98609-3 0  9999
2 62486  28.4591 236.2614 4457021 318.5961  15.0283  6.78689304 20144
Epoch: 2026-11-08T01:21Z
TLE epoch observation values (Epoch: 2026-11-08T01:21:00.776Z)
Latitude
-0.00006°
Longitude
168.75541°
Altitude
700.146 km
Speed
8.877 km/s
True Right ascension
15h 45m 02s
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
11:18:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,662.803 km
Perigee altitude
155.544 km
Semi-major axis
11,787.311 km
Eccentricity
0.4457
Inclination
28.4591°
RAAN
236.2614°
Arg. of periapsis
318.5961°
True anomaly
41.44998°
Mean anomaly
15.0283°
Eccentric anomaly
26.3715°
Mean motion
1.69598 °/min
Orbital period
212.27 mins
BSTAR
0.00098609
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

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