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 (12 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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-2C DEB
1 40265U 14059E   26295.72803955  .00001450  00000-0  47107-3 0  9991
2 40265  97.9153 358.3958 0162490  91.5909 270.3896 14.32901406626424
Epoch: 2026-10-22T17:28Z
TLE epoch observation values (Epoch: 2026-10-22T17:28:22.617Z)
Latitude
-0.00002°
Longitude
65.14279°
Altitude
786.106 km
Speed
7.46 km/s
True Right ascension
23h 53m 34s
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
13:18:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
895.451 km
Perigee altitude
662.854 km
Semi-major axis
7,157.29 km
Eccentricity
0.01625
Inclination
97.9153°
RAAN
358.3958°
Arg. of periapsis
91.5909°
True anomaly
268.52772°
Mean anomaly
270.3896°
Eccentric anomaly
269.45864°
Mean motion
3.58443 °/min
Orbital period
100.43 mins
BSTAR
0.00047107
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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