CZ-2C DEB, 40290

Orbit data source: Space-Track

CZ-2C DEB, 40290 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
40290, 2014-066E
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 (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: 23 hours ago

TLE from 23 hours ago
0 CZ-2C DEB
1 40290U 14066E   25260.14900812  .00016244  00000-0  17475-2 0  9995
2 40290  97.9125 230.0850 0054601  19.4931 340.8356 14.87474295579215
Epoch: 2025-09-17T03:34Z
TLE epoch observation values (Epoch: 2025-09-17T03:34:34.301Z)
Latitude
-0.00002°
Longitude
-179.88702°
Altitude
572.857 km
Speed
7.594 km/s
True Right ascension
15h 20m 20s
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
19:10:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.979 km
Perigee altitude
564.745 km
Semi-major axis
6,980.999 km
Eccentricity
0.00546
Inclination
97.9125°
RAAN
230.085°
Arg. of periapsis
19.4931°
True anomaly
340.62887°
Mean anomaly
340.8356°
Eccentric anomaly
340.73237°
Mean motion
3.72106 °/min
Orbital period
96.75 mins
BSTAR
0.0017475
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Other satellites on launch #66 in the year 2014 (2014-10-27 UTC)

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