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, 1.4 m
Radar Cross Section
7.676 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CZ-4C R/B
1 43278U 18034D   26033.27760241 -.00000019  00000-0  62982-4 0  9995
2 43278  63.4294 245.0281 0370694 358.4764   1.5110 13.60936615388481
Epoch: 2026-02-02T06:39Z
TLE epoch observation values (Epoch: 2026-02-02T06:39:44.848Z)
Latitude
-0.00004°
Longitude
12.61602°
Altitude
759.453 km
Speed
7.612 km/s
True Right ascension
16h 20m 06s
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
21:37:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,305.761 km
Perigee altitude
756.448 km
Semi-major axis
7,409.241 km
Eccentricity
0.03707
Inclination
63.4294°
RAAN
245.0281°
Arg. of periapsis
358.4764°
True anomaly
1.62844°
Mean anomaly
1.511°
Eccentric anomaly
1.56916°
Mean motion
3.40316 °/min
Orbital period
105.78 mins
BSTAR
0.000062982
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