CZ-2C DEB, 40288

Orbit data source: Space-Track

CZ-2C DEB, 40288 is space debris in SSO originally from a launch on Mon, 27 Oct 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
40288, 2014-066C
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)
2014-10-27 (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, 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 40288U 14066C   26121.27090034  .00001575  00000-0  52502-3 0  9991
2 40288  97.9624 245.3413 0156412 344.0521  15.5770 14.32148723597529
Epoch: 2026-05-01T06:30Z
TLE epoch observation values (Epoch: 2026-05-01T06:30:05.789Z)
Latitude
-0°
Longitude
-71.38838°
Altitude
679.702 km
Speed
7.573 km/s
True Right ascension
16h 21m 21s
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
01:46:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
893.652 km
Perigee altitude
669.676 km
Semi-major axis
7,159.801 km
Eccentricity
0.01564
Inclination
97.9624°
RAAN
245.3413°
Arg. of periapsis
344.0521°
True anomaly
16.06753°
Mean anomaly
15.577°
Eccentric anomaly
15.82133°
Mean motion
3.58255 °/min
Orbital period
100.49 mins
BSTAR
0.00052502
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Other satellites on launch #66 in the year 2014 (2014-10-27 UTC)

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