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, 5.5 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   26005.50741050  .00007121  00000-0  36364-3 0  9996
2 58200  97.7616  40.0333 0062155 194.7188 165.2237 15.15324913120196
Epoch: 2026-01-05T12:10Z
TLE epoch observation values (Epoch: 2026-01-05T12:10:40.267Z)
Latitude
0.00006°
Longitude
112.26194°
Altitude
564.55 km
Speed
7.556 km/s
True Right ascension
02h 40m 07s
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
19:08:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.836 km
Perigee altitude
474.123 km
Semi-major axis
6,895.117 km
Eccentricity
0.00622
Inclination
97.7616°
RAAN
40.0333°
Arg. of periapsis
194.7188°
True anomaly
165.404°
Mean anomaly
165.2237°
Eccentric anomaly
165.31398°
Mean motion
3.7908 °/min
Orbital period
94.97 mins
BSTAR
0.00036364
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Other satellites on launch #168 in the year 2023 (2023-10-31 UTC)

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