CZ-3C DEB, 39338
Orbit data source: Space-Track
CZ-3C DEB, 39338 is space debris in HEO originally from a launch on Sun, 31 Oct 2010 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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39338 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.4 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 CZ-3C DEB
1 39338U 10057C 25346.71309068 .00000344 00000-0 33621-2 0 9991
2 39338 20.0654 74.3099 7196145 218.2800 57.8013 2.25880766100189Epoch: 2025-12-12T17:06Z
TLE epoch observation values (Epoch: 2025-12-12T17:06:51.034Z)
Latitude
0.00002°
Longitude
95.93577°
Altitude
20,835.274 km
Speed
3.612 km/s
True Right ascension
04h 57m 11s
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
07:35:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,823.1 km
Perigee altitude
502.832 km
Semi-major axis
24,541.103 km
Eccentricity
0.71961
Inclination
20.0654°
RAAN
74.3099°
Arg. of periapsis
218.28°
True anomaly
141.67599°
Mean anomaly
57.8013°
Eccentric anomaly
98.57164°
Mean motion
0.56455 °/min
Orbital period
637.68 mins
BSTAR
0.0033621
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Other satellites on launch #57 in the year 2010 (2010-10-31 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-3C 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. |
|---|---|---|---|---|---|---|---|
| 186 mins | 2025-12-13 09:06:16.302Z | 152.926° SSE | 2025-12-13 10:36:16.302Z | 160.318° S | 41.55° | 2025-12-13 12:12:16.302Z | 109.296° ESE |
| 343 mins | 2025-12-14 03:22:16.302Z | 93.439° ESE | 2025-12-14 07:32:16.302Z | 102.9° ESE | 29.24° | 2025-12-14 09:05:16.302Z | 90.597° ESE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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