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 (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: 13 hours ago

TLE from 13 hours ago
0 CZ-2C DEB
1 40266U 14059F   26296.21656249  .00001315  00000-0  42288-3 0  9994
2 40266  98.3458 200.7986 0157865 198.5645 160.9741 14.34102689627022
Epoch: 2026-10-23T05:11Z
TLE epoch observation values (Epoch: 2026-10-23T05:11:50.999Z)
Latitude
-0.00003°
Longitude
91.19582°
Altitude
888.002 km
Speed
7.353 km/s
True Right ascension
13h 23m 11s
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
13:18:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
888.097 km
Perigee altitude
662.246 km
Semi-major axis
7,153.308 km
Eccentricity
0.01579
Inclination
98.3458°
RAAN
200.7986°
Arg. of periapsis
198.5645°
True anomaly
161.55301°
Mean anomaly
160.9741°
Eccentric anomaly
161.26462°
Mean motion
3.58742 °/min
Orbital period
100.35 mins
BSTAR
0.00042288
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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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