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
Last TLE update
16 hours ago
Origin
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

TLE from 16 hours ago
0 CZ-4C R/B
1 40112U 14047D   25199.67797922  .00000033  00000-0  61708-4 0  9991
2 40112  63.4154  81.9076 0528394 359.7381   0.3305 13.70168684547103
Epoch: 2025-07-18T16:16Z
TLE epoch observation values (Epoch: 2025-07-18T16:16:17.404Z)
Latitude
-0.00004°
Longitude
-98.89093°
Altitude
610.931 km
Speed
7.751 km/s
True Right ascension
05h 27m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
53.85784°
Longitude
36.30117°
Altitude
1,159.822 km
Speed
7.203 km/s
Apparent Right ascension
11h 47m 20s
Apparent Declination
15° 08' 54"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:23:23
Azimuth
321.044° NNW
Elevation
-25.553°
Doppler factor
1
Orbital elements
Apogee altitude
1,387.512 km
Perigee altitude
608.035 km
Semi-major axis
7,375.911 km
Eccentricity
0.05284
Inclination
63.4154°
RAAN
81.9076°
Arg. of periapsis
359.7381°
True anomaly
0.36789°
Mean anomaly
0.3305°
Eccentric anomaly
0.34894°
Mean motion
3.42626 °/min
Orbital period
105.07 mins
BSTAR
0.000061708
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