CZ-3B R/B, 58657

Orbit data source: Space-Track

CZ-3B R/B, 58657 is space debris in HEO originally from a launch on Tue, 26 Dec 2023 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
58657, 2023-207D
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)
2023-12-26 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-3B R/B
1 58657U 23207D   26171.31146562  .00001828  00000-0  76382-3 0  9998
2 58657  54.9711 279.1964 5515672 111.0564 314.6406  4.73009289 42166
Epoch: 2026-06-20T07:28Z
TLE epoch observation values (Epoch: 2026-06-20T07:28:30.629Z)
Latitude
-0°
Longitude
-101.47378°
Altitude
6,624.973 km
Speed
5.893 km/s
True Right ascension
18h 36m 43s
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
21:24:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,880.918 km
Perigee altitude
344.178 km
Semi-major axis
14,990.685 km
Eccentricity
0.55157
Inclination
54.9711°
RAAN
279.1964°
Arg. of periapsis
111.0564°
True anomaly
249.03827°
Mean anomaly
314.6406°
Eccentric anomaly
283.9733°
Mean motion
1.18253 °/min
Orbital period
304.43 mins
BSTAR
0.00076382
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Other satellites on launch #207 in the year 2023 (2023-12-26 UTC)

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