CZ-8A R/B, 62980

Orbit data source: Space-Track

CZ-8A R/B, 62980 is space debris in LEO originally from a launch on Tue, 11 Feb 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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
62980, 2025-030K
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-8A STAGE 2, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-02-11 (10 months ago)
Launch vehicle
Unknown
Launch site
Wenchang Satellite Launch Center (WSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.2 m
Radar Cross Section
36.967 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CZ-8A R/B
1 62980U 25030K   25354.42043596 -.00000015  00000-0  52130-4 0  9999
2 62980  50.0068 340.5496 0118124 106.3947 254.9993 14.32867780 44739
Epoch: 2025-12-20T10:05Z
TLE epoch observation values (Epoch: 2025-12-20T10:05:25.666Z)
Latitude
-0.00004°
Longitude
99.94513°
Altitude
805.512 km
Speed
7.44 km/s
True Right ascension
22h 42m 11s
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
22:20:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
867.49 km
Perigee altitude
698.312 km
Semi-major axis
7,161.038 km
Eccentricity
0.01181
Inclination
50.0068°
RAAN
340.5496°
Arg. of periapsis
106.3947°
True anomaly
253.69692°
Mean anomaly
254.9993°
Eccentric anomaly
254.3476°
Mean motion
3.58162 °/min
Orbital period
100.51 mins
BSTAR
0.00005213
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