CZ-4B R/B, 100657

Orbit data source: Space-Track

CZ-4B R/B, 100657 is space debris in LEO originally from a Chinese 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
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-09-10 (3 days ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 CZ-4B R/B
1 A0657U 26206G   26255.93303280  .00050385  00000-0  45406-3 0  9995
2 A0657  45.0893  93.7893 0160266   9.2969 351.0833 15.52711926   400
Epoch: 2026-09-12T22:23Z
TLE epoch observation values (Epoch: 2026-09-12T22:23:34.033Z)
Latitude
-0.00007°
Longitude
125.9625°
Altitude
301.419 km
Speed
7.789 km/s
True Right ascension
06h 15m 09s
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
20:48:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.222 km
Perigee altitude
301.627 km
Semi-major axis
6,788.561 km
Eccentricity
0.01603
Inclination
45.0893°
RAAN
93.7893°
Arg. of periapsis
9.2969°
True anomaly
350.7929°
Mean anomaly
351.0833°
Eccentric anomaly
350.93868°
Mean motion
3.8804 °/min
Orbital period
92.77 mins
BSTAR
0.00045406
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Other satellites on launch #205 in the year 2026 (2026-09-10 UTC)

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