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 (11 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
20.385 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 CZ-4C R/B
1 40112U 14047D   25341.18873996  .00000200  00000-0  12506-3 0  9999
2 40112  63.4142  60.6190 0542077 359.9828   0.1104 13.70271865566497
Epoch: 2025-12-07T04:31Z
TLE epoch observation values (Epoch: 2025-12-07T04:31:47.132Z)
Latitude
-0.00005°
Longitude
-83.53312°
Altitude
600.48 km
Speed
7.762 km/s
True Right ascension
04h 02m 28s
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
18:06:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,397.214 km
Perigee altitude
597.592 km
Semi-major axis
7,375.54 km
Eccentricity
0.05421
Inclination
63.4142°
RAAN
60.619°
Arg. of periapsis
359.9828°
True anomaly
0.12324°
Mean anomaly
0.1104°
Eccentric anomaly
0.11673°
Mean motion
3.42651 °/min
Orbital period
105.06 mins
BSTAR
0.00012506
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