CZ-3B R/B, 69571

Orbit data source: Space-Track

CZ-3B R/B, 69571 is space debris in HEO originally from a launch on Tue, 16 Jun 2026 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
69571, 2026-136B
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)
2026-06-16 (3 days ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CZ-3B R/B
1 69571U 26136B   26168.13176650  .00174117 -12277-4  22190-3 0  9990
2 69571  63.4344 355.9302 7369172 171.4047 217.7535  2.23819647    35
Epoch: 2026-06-17T03:09Z
TLE epoch observation values (Epoch: 2026-06-17T03:09:44.625Z)
Latitude
0.00005°
Longitude
43.11208°
Altitude
35,157.959 km
Speed
1.746 km/s
True Right ascension
23h 43m 46s
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
05:54:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,499.295 km
Perigee altitude
116.309 km
Semi-major axis
24,685.939 km
Eccentricity
0.73692
Inclination
63.4344°
RAAN
355.9302°
Arg. of periapsis
171.4047°
True anomaly
188.63729°
Mean anomaly
217.7535°
Eccentric anomaly
201.96244°
Mean motion
0.55959 °/min
Orbital period
643.33 mins
BSTAR
0.0002219
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Other satellites on launch #136 in the year 2026 (2026-06-16 UTC)

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