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: 10 hours ago

TLE from 10 hours ago
0 CZ-4C R/B
1 40112U 14047D   26103.96831230  .00000209  00000-0  12285-3 0  9990
2 40112  63.4101  76.1347 0554652   0.2604 359.8622 13.70372970584003
Epoch: 2026-04-13T23:14Z
TLE epoch observation values (Epoch: 2026-04-13T23:14:22.182Z)
Latitude
0.00002°
Longitude
-114.60902°
Altitude
590.86 km
Speed
7.772 km/s
True Right ascension
05h 04m 32s
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
15:20:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,406.106 km
Perigee altitude
587.975 km
Semi-major axis
7,375.177 km
Eccentricity
0.05547
Inclination
63.4101°
RAAN
76.1347°
Arg. of periapsis
0.2604°
True anomaly
359.84578°
Mean anomaly
359.8622°
Eccentric anomaly
359.85411°
Mean motion
3.42677 °/min
Orbital period
105.06 mins
BSTAR
0.00012285
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