CZ-2D DEB, 38301 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 38301 was space debris in SSO originally from a launch on Tue, 15 Jun 2010 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
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CZ-2D DEB
1 38301U 10027F 25335.39845226 .00733523 00000-0 41526-2 0 9995
2 38301 97.6003 209.3772 0020239 110.8312 249.5124 15.76888339818972Epoch: 2025-12-01T09:33Z
TLE epoch observation values (Epoch: 2025-12-01T09:33:46.275Z)
Latitude
0.00006°
Longitude
-4.56414°
Altitude
347.208 km
Speed
7.698 km/s
True Right ascension
13h 57m 30s
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
00:27:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
349.751 km
Perigee altitude
322.573 km
Semi-major axis
6,714.299 km
Eccentricity
0.00202
Inclination
97.6003°
RAAN
209.3772°
Arg. of periapsis
110.8312°
True anomaly
249.29534°
Mean anomaly
249.5124°
Eccentric anomaly
249.40385°
Mean motion
3.94496 °/min
Orbital period
91.26 mins
BSTAR
0.0041526
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Other satellites on launch #27 in the year 2010 (2010-06-15 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-2D DEB 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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