CZ-6A R/B, 58200

Orbit data source: Space-Track

CZ-6A R/B, 58200 is space debris in SSO originally from a launch on Tue, 31 Oct 2023 UTC launched from the Taiyaun Space Center, China (TSC). 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
58200, 2023-168B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-6A STAGE 2, YF-115
Mass
~6,000 kg wet, ~6,000 kg dry
Launch date (UTC)
2023-10-31 (3 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 4.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 CZ-6A R/B
1 58200U 23168B   26275.28657142  .00002225  00000-0  10943-3 0  9993
2 58200  97.7308 315.5693 0058976 346.9923  12.9785 15.17646046161082
Epoch: 2026-10-02T06:52Z
TLE epoch observation values (Epoch: 2026-10-02T06:52:39.770Z)
Latitude
-0.00007°
Longitude
-158.6071°
Altitude
476.436 km
Speed
7.649 km/s
True Right ascension
21h 02m 16s
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
07:25:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.563 km
Perigee altitude
469.317 km
Semi-major axis
6,888.077 km
Eccentricity
0.0059
Inclination
97.7308°
RAAN
315.5693°
Arg. of periapsis
346.9923°
True anomaly
13.13138°
Mean anomaly
12.9785°
Eccentric anomaly
13.05483°
Mean motion
3.79661 °/min
Orbital period
94.82 mins
BSTAR
0.00010943
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Other satellites on launch #168 in the year 2023 (2023-10-31 UTC)

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