CZ-2D R/B, 54215

Orbit data source: Space-Track

CZ-2D R/B, 54215 is space debris in LEO originally from a launch on Sat, 29 Oct 2022 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
54215, 2022-142B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
BWYIC
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
2022-10-29 (4 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
27.824 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-2D R/B
1 54215U 22142B   26171.46102102 -.00000033  00000-0  37261-4 0  9991
2 54215  59.9006 241.6426 0020141 273.3600  86.5132 14.34370793190817
Epoch: 2026-06-20T11:03Z
TLE epoch observation values (Epoch: 2026-06-20T11:03:52.216Z)
Latitude
-0.00003°
Longitude
166.9997°
Altitude
777.837 km
Speed
7.466 km/s
True Right ascension
16h 06m 34s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:33:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.817 km
Perigee altitude
761.997 km
Semi-major axis
7,154.544 km
Eccentricity
0.00201
Inclination
59.9006°
RAAN
241.6426°
Arg. of periapsis
273.36°
True anomaly
86.74361°
Mean anomaly
86.5132°
Eccentric anomaly
86.6284°
Mean motion
3.58649 °/min
Orbital period
100.38 mins
BSTAR
0.000037261
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Other satellites on launch #142 in the year 2022 (2022-10-29 UTC)

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