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: 7 hours ago

TLE from 7 hours ago
0 CZ-4C R/B
1 40112U 14047D   25289.15474725  .00000495  00000-0  24608-3 0  9996
2 40112  63.4134 200.8463 0537222 359.8746   0.2075 13.70237191559363
Epoch: 2025-10-16T03:42Z
TLE epoch observation values (Epoch: 2025-10-16T03:42:50.162Z)
Latitude
-0.00006°
Longitude
120.21872°
Altitude
604.181 km
Speed
7.758 km/s
True Right ascension
13h 23m 23s
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
04:58:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,393.765 km
Perigee altitude
601.291 km
Semi-major axis
7,375.665 km
Eccentricity
0.05372
Inclination
63.4134°
RAAN
200.8463°
Arg. of periapsis
359.8746°
True anomaly
0.23139°
Mean anomaly
0.2075°
Eccentric anomaly
0.21928°
Mean motion
3.42643 °/min
Orbital period
105.07 mins
BSTAR
0.00024608
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