CZ-2C DEB, 40263

Orbit data source: Space-Track

CZ-2C DEB, 40263 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
40263, 2014-059C
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: 12 hours ago

TLE from 12 hours ago
0 CZ-2C DEB
1 40263U 14059C   26296.27457822  .00019285  00000-0  17242-2 0  9999
2 40263  98.2041  55.1073 0051204 220.8549 138.8827 14.94915650642197
Epoch: 2026-10-23T06:35Z
TLE epoch observation values (Epoch: 2026-10-23T06:35:23.558Z)
Latitude
-0.00005°
Longitude
-75.43832°
Altitude
612.603 km
Speed
7.538 km/s
True Right ascension
03h 40m 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
13:17:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.296 km
Perigee altitude
544.043 km
Semi-major axis
6,957.806 km
Eccentricity
0.00512
Inclination
98.2041°
RAAN
55.1073°
Arg. of periapsis
220.8549°
True anomaly
139.2667°
Mean anomaly
138.8827°
Eccentric anomaly
139.07488°
Mean motion
3.73968 °/min
Orbital period
96.26 mins
BSTAR
0.0017242
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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