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 (11 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.751 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 CZ-3A R/B
1 40368U 14090B   25338.45285391  .00006618  00000-0  37190-2 0  9996
2 40368  24.2500 111.3507 7285303 118.4237 331.3618  2.25676573 87922
Epoch: 2025-12-04T10:52Z
TLE epoch observation values (Epoch: 2025-12-04T10:52:06.577Z)
Latitude
-0°
Longitude
-125.29898°
Altitude
11,265.349 km
Speed
5.38 km/s
True Right ascension
07h 24m 57s
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
06:16:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,067.057 km
Perigee altitude
287.979 km
Semi-major axis
24,555.655 km
Eccentricity
0.72853
Inclination
24.25°
RAAN
111.3507°
Arg. of periapsis
118.4237°
True anomaly
241.73899°
Mean anomaly
331.3618°
Eccentric anomaly
292.91388°
Mean motion
0.56405 °/min
Orbital period
638.24 mins
BSTAR
0.003719
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Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

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