CZ-6A R/B, 60214
Orbit data source: Space-Track
CZ-6A R/B, 60214 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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60214 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CZ-6A R/B
1 60214U 24126D 25261.05081349 .00004184 00000-0 23836-3 0 9996
2 60214 97.8059 281.2133 0070787 332.9498 26.8049 15.11270773 66296Epoch: 2025-09-18T01:13Z
TLE epoch observation values (Epoch: 2025-09-18T01:13:10.285Z)
Latitude
-0°
Longitude
-94.29752°
Altitude
491.791 km
Speed
7.643 km/s
True Right ascension
18h 44m 51s
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
08:52:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.214 km
Perigee altitude
480.422 km
Semi-major axis
6,907.455 km
Eccentricity
0.00708
Inclination
97.8059°
RAAN
281.2133°
Arg. of periapsis
332.9498°
True anomaly
27.1736°
Mean anomaly
26.8049°
Eccentric anomaly
26.98896°
Mean motion
3.78065 °/min
Orbital period
95.22 mins
BSTAR
0.00023836
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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 R/B 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-19 01:11:06.881Z | 149.163° SSE | 2025-09-19 01:14:06.881Z | 72.017° E | 39.009° | 2025-09-19 01:17:06.881Z | 359.427° N |
| 7 mins | 2025-09-19 14:20:06.881Z | 12.448° NNE | 2025-09-19 14:23:06.881Z | 206.549° SW | 44.992° | 2025-09-19 14:27:06.881Z | 193.763° SSW |
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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