CZ-3A R/B, 26383

Orbit data source: Space-Track

CZ-3A R/B, 26383 is space debris in HEO originally from a launch on Sun, 25 Jun 2000 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
26383, 2000-032B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3 STAGE 3, Unknown motor
Mass
~2,000 kg wet, 2,000 kg dry
Launch date (UTC)
2000-06-25 (26 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.8 m
Radar Cross Section
15.242 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-3A R/B
1 26383U 00032B   26073.55002182  .00009368  00000-0  13748-2 0  9999
2 26383  27.2670 142.9450 5800234  33.2542 352.5124  4.35918961 31253
Epoch: 2026-03-14T13:12Z
TLE epoch observation values (Epoch: 2026-03-14T13:12:01.885Z)
Latitude
0.00011°
Longitude
132.79989°
Altitude
685.506 km
Speed
9.364 km/s
True Right ascension
09h 31m 54s
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
18:01:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,638.286 km
Perigee altitude
271.329 km
Semi-major axis
15,832.945 km
Eccentricity
0.58002
Inclination
27.267°
RAAN
142.945°
Arg. of periapsis
33.2542°
True anomaly
326.83315°
Mean anomaly
352.5124°
Eccentric anomaly
342.5427°
Mean motion
1.08943 °/min
Orbital period
330.45 mins
BSTAR
0.0013748
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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

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