CZ-4C R/B, 43278

Orbit data source: Space-Track

CZ-4C R/B, 43278 is space debris in LEO originally from a launch on Tue, 10 Apr 2018 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
43278, 2018-034D
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)
2018-04-10 (8 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
14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 CZ-4C R/B
1 43278U 18034D   26123.36231279 -.00000042  00000-0  42841-4 0  9997
2 43278  63.4325   6.9510 0379132 358.3799   1.5978 13.60948950400749
Epoch: 2026-05-03T08:41Z
TLE epoch observation values (Epoch: 2026-05-03T08:41:43.825Z)
Latitude
-0.00005°
Longitude
15.25142°
Altitude
753.172 km
Speed
7.619 km/s
True Right ascension
00h 27m 48s
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
03:49:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,311.965 km
Perigee altitude
750.153 km
Semi-major axis
7,409.196 km
Eccentricity
0.03791
Inclination
63.4325°
RAAN
6.951°
Arg. of periapsis
358.3799°
True anomaly
1.72495°
Mean anomaly
1.5978°
Eccentric anomaly
1.66076°
Mean motion
3.40319 °/min
Orbital period
105.78 mins
BSTAR
0.000042841
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