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: 6 days ago

TLE from 6 days ago
0 CZ-3A R/B
1 26383U 00032B   25345.93385627  .00010651  00000-0  11659-2 0  9996
2 26383  27.2720 220.5311 5820396 264.6140  30.3972  4.34160307 27229
Epoch: 2025-12-11T22:24Z
TLE epoch observation values (Epoch: 2025-12-11T22:24:45.181Z)
Latitude
0.00013°
Longitude
163.49739°
Altitude
4,737.341 km
Speed
6.827 km/s
True Right ascension
14h 42m 16s
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
03:02:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,737.804 km
Perigee altitude
257.265 km
Semi-major axis
15,875.671 km
Eccentricity
0.58204
Inclination
27.272°
RAAN
220.5311°
Arg. of periapsis
264.614°
True anomaly
95.46152°
Mean anomaly
30.3972°
Eccentric anomaly
58.97482°
Mean motion
1.08504 °/min
Orbital period
331.79 mins
BSTAR
0.0011659
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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

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