CZ-2C DEB, 40266

Orbit data source: Space-Track

CZ-2C DEB, 40266 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
40266, 2014-059F
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: 1 day ago

TLE from 1 day ago
0 CZ-2C DEB
1 40266U 14059F   26022.55950829  .00004511  00000-0  14412-2 0  9997
2 40266  98.3604 296.4209 0160959 294.0590  64.3825 14.33003260587810
Epoch: 2026-01-22T13:25Z
TLE epoch observation values (Epoch: 2026-01-22T13:25:41.516Z)
Latitude
-0°
Longitude
-26.91301°
Altitude
736.341 km
Speed
7.512 km/s
True Right ascension
19h 45m 41s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
20:56:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
894.031 km
Perigee altitude
663.635 km
Semi-major axis
7,156.97 km
Eccentricity
0.0161
Inclination
98.3604°
RAAN
296.4209°
Arg. of periapsis
294.059°
True anomaly
66.05999°
Mean anomaly
64.3825°
Eccentric anomaly
65.21981°
Mean motion
3.58467 °/min
Orbital period
100.43 mins
BSTAR
0.0014412
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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