CZ-3B R/B, 67247
Orbit data source: Space-Track
CZ-3B R/B, 67247 is space debris originally from a launch on Fri, 26 Dec 2025 UTC launched from the Xichang Space Center, China (XSC). 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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67247 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 8.0 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 CZ-3B R/B
1 67247U 25312B 26151.57957803 .05321609 -30377-5 95363-3 0 9999
2 67247 28.1572 212.3369 4187483 18.3057 353.1364 7.35094684 6117Epoch: 2026-05-31T13:54Z
TLE epoch observation values (Epoch: 2026-05-31T13:54:35.541Z)
Latitude
-0.00005°
Longitude
114.60949°
Altitude
213.139 km
Speed
9.235 km/s
True Right ascension
14h 09m 20s
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
07:20:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,478.638 km
Perigee altitude
118.278 km
Semi-major axis
11,176.595 km
Eccentricity
0.41875
Inclination
28.1572°
RAAN
212.3369°
Arg. of periapsis
18.3057°
True anomaly
341.73576°
Mean anomaly
353.1364°
Eccentric anomaly
348.25089°
Mean motion
1.83687 °/min
Orbital period
195.99 mins
BSTAR
0.00095363
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Other satellites on launch #312 in the year 2025 (2025-12-26 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-3B 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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| CZ-3B R/B is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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