DECAYED

ZK-1A R/B, 67002 (Decayed)

Orbit data source: Space-Track

ZK-1A R/B, 67002 was space debris in LEO originally from a launch on Wed, 10 Dec 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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.

Not visible in the next 10 days
Identifier
67002, 2025-292K
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAS
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
2025-12-10 (6 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
5.880 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 months ago

TLE from 4 months ago
0 ZK-1A R/B
1 67002U 25292K   26063.80659399  .09853770  27510-5  27722-3 0  9993
2 67002  97.6751 150.8442 0018268  50.8093 309.4826 16.43602557 13326
Epoch: 2026-03-04T19:21Z
TLE epoch observation values (Epoch: 2026-03-04T19:21:29.720Z)
Latitude
-0.00008°
Longitude
57.90436°
Altitude
151.905 km
Speed
7.82 km/s
True Right ascension
10h 03m 22s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:32:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.983 km
Perigee altitude
141.121 km
Semi-major axis
6,531.189 km
Eccentricity
0.00183
Inclination
97.6751°
RAAN
150.8442°
Arg. of periapsis
50.8093°
True anomaly
309.3208°
Mean anomaly
309.4826°
Eccentric anomaly
309.40172°
Mean motion
4.11202 °/min
Orbital period
87.55 mins
BSTAR
0.00027722
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