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: 12 hours ago

TLE from 12 hours ago
0 CZ-2C DEB
1 40266U 14059F   26061.72687695  .00002146  00000-0  69067-3 0  9996
2 40266  98.3597 334.2571 0159859 176.5618 183.6706 14.33251059593424
Epoch: 2026-03-02T17:26Z
TLE epoch observation values (Epoch: 2026-03-02T17:26:42.168Z)
Latitude
-0.00002°
Longitude
-87.93474°
Altitude
898.068 km
Speed
7.344 km/s
True Right ascension
22h 17m 01s
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
09:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
892.405 km
Perigee altitude
663.61 km
Semi-major axis
7,156.145 km
Eccentricity
0.01599
Inclination
98.3597°
RAAN
334.2571°
Arg. of periapsis
176.5618°
True anomaly
183.55562°
Mean anomaly
183.6706°
Eccentric anomaly
183.61288°
Mean motion
3.58529 °/min
Orbital period
100.41 mins
BSTAR
0.00069067
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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