CZ-4B R/B, 100657

Orbit data source: Space-Track

CZ-4B R/B, 100657 is space debris in LEO originally from a launch on Thu, 10 Sep 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
100657, 2026-205G
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2026-09-10 (1 month ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 8.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 CZ-4B R/B
1 A0657U 26205G   26287.03788391  .00065449  98691-5  55724-3 0  9999
2 A0657  45.0897 277.1569 0150702 195.7750 163.8421 15.56156617  5248
Epoch: 2026-10-14T00:54Z
TLE epoch observation values (Epoch: 2026-10-14T00:54:33.169Z)
Latitude
-0.00007°
Longitude
-119.07472°
Altitude
497.001 km
Speed
7.563 km/s
True Right ascension
18h 28m 37s
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
14:21:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.561 km
Perigee altitude
298.253 km
Semi-major axis
6,778.544 km
Eccentricity
0.01507
Inclination
45.0897°
RAAN
277.1569°
Arg. of periapsis
195.775°
True anomaly
164.31412°
Mean anomaly
163.8421°
Eccentric anomaly
164.07896°
Mean motion
3.88901 °/min
Orbital period
92.57 mins
BSTAR
0.00055724
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Other satellites on launch #205 in the year 2026 (2026-09-10 UTC)

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