CZ-6A DEB, 60213
Orbit data source: Space-Track
CZ-6A DEB, 60213 is space debris in SSO originally from a launch on Thu, 04 Jul 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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60213 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 0.3 m
Radar Cross Section
0.159 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CZ-6A DEB
1 60213U 24126C 25309.98022780 .00016455 00000-0 11971-2 0 9994
2 60213 97.8349 322.1527 0004923 338.2037 21.8978 15.03879961 73116Epoch: 2025-11-05T23:31Z
TLE epoch observation values (Epoch: 2025-11-05T23:31:31.681Z)
Latitude
-0.00005°
Longitude
-76.17442°
Altitude
554.834 km
Speed
7.586 km/s
True Right ascension
21h 28m 36s
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
04:52:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.364 km
Perigee altitude
548.54 km
Semi-major axis
6,930.089 km
Eccentricity
0.00049
Inclination
97.8349°
RAAN
322.1527°
Arg. of periapsis
338.2037°
True anomaly
21.91885°
Mean anomaly
21.8978°
Eccentric anomaly
21.90832°
Mean motion
3.76214 °/min
Orbital period
95.69 mins
BSTAR
0.0011971
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Other satellites on launch #126 in the year 2024 (2024-07-04 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-6A DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-06 12:53:00.770Z | 51.907° ENE | 2025-11-06 12:56:00.770Z | 102.168° ESE | 16.789° | 2025-11-06 12:58:00.770Z | 134.109° SE |
| 5 mins | 2025-11-06 14:28:00.770Z | 342.398° N | 2025-11-06 14:30:00.770Z | 302.438° NW | 27.092° | 2025-11-06 14:33:00.770Z | 234.068° WSW |
| 6 mins | 2025-11-07 01:12:00.770Z | 181.475° SSW | 2025-11-07 01:15:00.770Z | 255.533° W | 40.752° | 2025-11-07 01:18:00.770Z | 336.463° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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