CZ-3A R/B, 38050

Orbit data source: Space-Track

CZ-3A R/B, 38050 is space debris in HEO originally from a launch on Fri, 13 Jan 2012 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
38050, 2012-002B
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)
2012-01-13 (14 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
32.751 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 CZ-3A R/B
1 38050U 12002B   26133.63807326  .00000048  00000-0  27032-3 0  9990
2 38050  24.8453 316.4131 7204157 309.6449   6.1697  2.32895222120236
Epoch: 2026-05-13T15:18Z
TLE epoch observation values (Epoch: 2026-05-13T15:18:49.529Z)
Latitude
0.0003°
Longitude
-144.71914°
Altitude
1,550.247 km
Speed
9.163 km/s
True Right ascension
21h 05m 31s
True Declination
0° 00' 01"
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
17:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,990.199 km
Perigee altitude
344.62 km
Semi-major axis
24,045.547 km
Eccentricity
0.72042
Inclination
24.8453°
RAAN
316.4131°
Arg. of periapsis
309.6449°
True anomaly
49.13539°
Mean anomaly
6.1697°
Eccentric anomaly
20.88378°
Mean motion
0.58209 °/min
Orbital period
618.46 mins
BSTAR
0.00027032
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Other satellites on launch #2 in the year 2012 (2012-01-13 UTC)

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