CZ-3A R/B, 40368

Orbit data source: Space-Track

CZ-3A R/B, 40368 is space debris in HEO originally from a launch on Wed, 31 Dec 2014 UTC launched from the Xichang Space Center, China (XSC). 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
40368, 2014-090B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2014-12-31 (12 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3A R/B
1 40368U 14090B   26295.31823869  .00000404  00000-0  52010-3 0  9998
2 40368  25.0506 353.1468 7256044 321.3744   4.6917  2.26479375 95212
Epoch: 2026-10-22T07:38Z
TLE epoch observation values (Epoch: 2026-10-22T07:38:15.822Z)
Latitude
0.00013°
Longitude
-152.16249°
Altitude
1,045.612 km
Speed
9.545 km/s
True Right ascension
23h 32m 37s
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
20:37:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,894.803 km
Perigee altitude
343.861 km
Semi-major axis
24,497.469 km
Eccentricity
0.7256
Inclination
25.0506°
RAAN
353.1468°
Arg. of periapsis
321.3744°
True anomaly
39.95834°
Mean anomaly
4.6917°
Eccentric anomaly
16.49794°
Mean motion
0.56606 °/min
Orbital period
635.98 mins
BSTAR
0.0005201
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Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

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