CZ-2C DEB, 40265

Orbit data source: Space-Track

CZ-2C DEB, 40265 is space debris in SSO originally from a launch on Sun, 28 Sep 2014 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
40265, 2014-059E
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2014-09-28 (11 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 CZ-2C DEB
1 40265U 14059E   25342.47130402  .00003922  00000-0  12881-2 0  9991
2 40265  97.9407  67.1065 0162592 328.0000  31.1390 14.31570039580865
Epoch: 2025-12-08T11:18Z
TLE epoch observation values (Epoch: 2025-12-08T11:18:40.667Z)
Latitude
-0.00005°
Longitude
179.9672°
Altitude
690.234 km
Speed
7.563 km/s
True Right ascension
04h 28m 25s
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
18:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.038 km
Perigee altitude
667.15 km
Semi-major axis
7,161.731 km
Eccentricity
0.01626
Inclination
97.9407°
RAAN
67.1065°
Arg. of periapsis
328°
True anomaly
32.11947°
Mean anomaly
31.139°
Eccentric anomaly
31.62752°
Mean motion
3.5811 °/min
Orbital period
100.53 mins
BSTAR
0.0012881
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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