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 (2 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 2.8 m
Radar Cross Section
5.500 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 CZ-6A R/B
1 58200U 23168B   25260.96737635  .00004097  00000-0  21989-3 0  9998
2 58200  97.7768 288.2013 0063842 211.1514 148.5927 15.13781792103614
Epoch: 2025-09-17T23:13Z
TLE epoch observation values (Epoch: 2025-09-17T23:13:01.316Z)
Latitude
0.00004°
Longitude
-57.18992°
Altitude
565.447 km
Speed
7.558 km/s
True Right ascension
19h 12m 48s
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
21:24:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.719 km
Perigee altitude
477.62 km
Semi-major axis
6,899.807 km
Eccentricity
0.00638
Inclination
97.7768°
RAAN
288.2013°
Arg. of periapsis
211.1514°
True anomaly
148.97135°
Mean anomaly
148.5927°
Eccentric anomaly
148.78228°
Mean motion
3.78693 °/min
Orbital period
95.06 mins
BSTAR
0.00021989
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Other satellites on launch #168 in the year 2023 (2023-10-31 UTC)

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