CZ-4B R/B, 67301 (Decayed)
Orbit data source: Space-Track
CZ-4B R/B, 67301 was space debris in LEO originally from a launch on Tue, 30 Dec 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
14.536 m²
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 CZ-4B R/B
1 67301U 25314B 26094.03971603 .13220197 24912-5 16564-3 0 9995
2 67301 97.3460 178.3729 0011405 328.2292 31.8323 16.49157208 14989Epoch: 2026-04-04T00:57Z
TLE epoch observation values (Epoch: 2026-04-04T00:57:11.464Z)
Latitude
-0.00006°
Longitude
-28.29007°
Altitude
138.504 km
Speed
7.827 km/s
True Right ascension
11h 53m 29s
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
15:33:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.781 km
Perigee altitude
130.917 km
Semi-major axis
6,516.486 km
Eccentricity
0.00114
Inclination
97.346°
RAAN
178.3729°
Arg. of periapsis
328.2292°
True anomaly
31.90131°
Mean anomaly
31.8323°
Eccentric anomaly
31.8668°
Mean motion
4.12594 °/min
Orbital period
87.25 mins
BSTAR
0.00016564
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Other satellites on launch #314 in the year 2025 (2025-12-30 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-4B 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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