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, 3.9 m
Radar Cross Section
15.242 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-3A R/B
1 26383U 00032B   26252.57740298  .00004059  00000-0  64983-3 0  9997
2 26383  27.4293 352.2708 5779132 282.7727  21.6354  4.38434675 39093
Epoch: 2026-09-09T13:51Z
TLE epoch observation values (Epoch: 2026-09-09T13:51:27.617Z)
Latitude
0.00009°
Longitude
155.77999°
Altitude
2,942.772 km
Speed
7.762 km/s
True Right ascension
23h 29m 05s
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
05:42:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,509.2 km
Perigee altitude
279.147 km
Semi-major axis
15,772.311 km
Eccentricity
0.57791
Inclination
27.4293°
RAAN
352.2708°
Arg. of periapsis
282.7727°
True anomaly
77.49526°
Mean anomaly
21.6354°
Eccentric anomaly
45.08301°
Mean motion
1.09572 °/min
Orbital period
328.55 mins
BSTAR
0.00064983
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Other satellites on launch #32 in the year 2000 (2000-06-25 UTC)

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