CZ-3B R/B, 43247

Orbit data source: Space-Track

CZ-3B R/B, 43247 is space debris in HEO originally from a launch on Thu, 29 Mar 2018 UTC launched from the Xichang Space Center, China (XSC). 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
43247, 2018-029C
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2018-03-29 (8 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CZ-3B R/B
1 43247U 18029C   26170.20179171  .00003087  00000-0  96391-3 0  9993
2 43247  54.9016  87.3975 5530951  83.5710 333.4827  4.72528070140581
Epoch: 2026-06-19T04:50Z
TLE epoch observation values (Epoch: 2026-06-19T04:50:34.803Z)
Latitude
0.00004°
Longitude
107.32746°
Altitude
3,419.123 km
Speed
7.403 km/s
True Right ascension
05h 49m 37s
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
23:08:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,919.64 km
Perigee altitude
325.825 km
Semi-major axis
15,000.869 km
Eccentricity
0.5531
Inclination
54.9016°
RAAN
87.3975°
Arg. of periapsis
83.571°
True anomaly
276.43093°
Mean anomaly
333.4827°
Eccentric anomaly
308.77776°
Mean motion
1.18132 °/min
Orbital period
304.74 mins
BSTAR
0.00096391
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Other satellites on launch #29 in the year 2018 (2018-03-29 UTC)

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