CZ-4C R/B, 40112

Orbit data source: Space-Track

CZ-4C R/B, 40112 is space debris in LEO originally from a launch on Sat, 09 Aug 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
40112, 2014-047D
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2014-08-09 (12 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.5 m
Radar Cross Section
20.385 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-4C R/B
1 40112U 14047D   26171.39430403 -.00000029  00000-0  33415-4 0  9999
2 40112  63.4098 254.2955 0561197   0.4201 359.7198 13.70401434593240
Epoch: 2026-06-20T09:27Z
TLE epoch observation values (Epoch: 2026-06-20T09:27:47.868Z)
Latitude
-0.00007°
Longitude
-156.26354°
Altitude
585.94 km
Speed
7.777 km/s
True Right ascension
16h 57m 10s
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
21:36:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.825 km
Perigee altitude
583.051 km
Semi-major axis
7,375.075 km
Eccentricity
0.05612
Inclination
63.4098°
RAAN
254.2955°
Arg. of periapsis
0.4201°
True anomaly
359.68599°
Mean anomaly
359.7198°
Eccentric anomaly
359.70314°
Mean motion
3.42684 °/min
Orbital period
105.05 mins
BSTAR
0.000033415
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