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 (25 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: 19 hours ago

TLE from 19 hours ago
0 CZ-3A R/B
1 26383U 00032B   25258.15922137  .00009114  00000-0  13163-2 0  9990
2 26383  27.3350 293.5271 5822331 143.7750 275.2197  4.32496510 23411
Epoch: 2025-09-15T03:49Z
TLE epoch observation values (Epoch: 2025-09-15T03:49:16.726Z)
Latitude
-0.00004°
Longitude
-118.14141°
Altitude
13,447.102 km
Speed
3.894 km/s
True Right ascension
19h 34m 11s
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
15:49:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,805.219 km
Perigee altitude
271.182 km
Semi-major axis
15,916.338 km
Eccentricity
0.58223
Inclination
27.335°
RAAN
293.5271°
Arg. of periapsis
143.775°
True anomaly
216.24477°
Mean anomaly
275.2197°
Eccentric anomaly
244.98855°
Mean motion
1.08088 °/min
Orbital period
333.06 mins
BSTAR
0.0013163
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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

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