CZ-6C R/B, 59681 (Decayed)
Orbit data source: Space-Track
CZ-6C R/B, 59681 was space debris in LEO originally from a launch on Tue, 07 May 2024 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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59681 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
CZ-6 STAGE 2, Unknown motor
Mass
3,000 kg wet, 3,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.0 m
Radar Cross Section
21.524 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 CZ-6C R/B
1 59681U 24085E 26022.81715313 .11615887 25870-5 11480-3 0 9990
2 59681 97.2986 126.2654 0009913 243.1356 116.8937 16.50840862 97274Epoch: 2026-01-22T19:36Z
TLE epoch observation values (Epoch: 2026-01-22T19:36:42.030Z)
Latitude
0.00002°
Longitude
69.92539°
Altitude
143.318 km
Speed
7.818 km/s
True Right ascension
08h 25m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:20:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
140.367 km
Perigee altitude
127.456 km
Semi-major axis
6,512.048 km
Eccentricity
0.00099
Inclination
97.2986°
RAAN
126.2654°
Arg. of periapsis
243.1356°
True anomaly
116.99495°
Mean anomaly
116.8937°
Eccentric anomaly
116.94433°
Mean motion
4.13016 °/min
Orbital period
87.16 mins
BSTAR
0.0001148
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Other satellites on launch #85 in the year 2024 (2024-05-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-6C R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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