ZK-1A R/B, 64093

Orbit data source: Space-Track

ZK-1A R/B, 64093 is space debris in SSO originally from a launch on Wed, 21 May 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.

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Identifier
64093, 2025-108G
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAS
Mission
Spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
2025-05-21 (1 year ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.0 m
Radar Cross Section
5.880 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 ZK-1A R/B
1 64093U 25108G   26171.40074286  .00028117  00000-0  35339-3 0  9991
2 64093  97.4282 262.0230 0066283  26.7680 333.6970 15.56956159 60970
Epoch: 2026-06-20T09:37Z
TLE epoch observation values (Epoch: 2026-06-20T09:37:04.183Z)
Latitude
-0.00002°
Longitude
-150.86033°
Altitude
359.407 km
Speed
7.716 km/s
True Right ascension
17h 28m 05s
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
07:19:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
438.273 km
Perigee altitude
348.506 km
Semi-major axis
6,771.527 km
Eccentricity
0.00663
Inclination
97.4282°
RAAN
262.023°
Arg. of periapsis
26.768°
True anomaly
333.35792°
Mean anomaly
333.697°
Eccentric anomaly
333.52771°
Mean motion
3.89505 °/min
Orbital period
92.42 mins
BSTAR
0.00035339
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Other satellites on launch #108 in the year 2025 (2025-05-21 UTC)

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