CZ-2D DEB, 43403
Orbit data source: Space-Track
CZ-2D DEB, 43403 is space debris in SSO originally from a launch on Sat, 29 Sep 2012 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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43403 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CZ-2D DEB
1 43403U 12052C 25258.53589192 .00002014 00000-0 51413-3 0 9992
2 43403 98.0233 0.8896 0194656 54.0217 307.8850 14.40753895616721Epoch: 2025-09-15T12:51Z
TLE epoch observation values (Epoch: 2025-09-15T12:51:41.061Z)
Latitude
-0.0001°
Longitude
173.22938°
Altitude
675.393 km
Speed
7.563 km/s
True Right ascension
00h 03m 33s
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
00:13:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
891.92 km
Perigee altitude
614.292 km
Semi-major axis
7,131.243 km
Eccentricity
0.01947
Inclination
98.0233°
RAAN
0.8896°
Arg. of periapsis
54.0217°
True anomaly
306.09812°
Mean anomaly
307.885°
Eccentric anomaly
306.99422°
Mean motion
3.60409 °/min
Orbital period
99.89 mins
BSTAR
0.00051413
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Other satellites on launch #52 in the year 2012 (2012-09-29 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 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-16 19:25:33.708Z | 24.584° NE | 2025-09-16 19:29:33.708Z | 94.698° ESE | 39.113° | 2025-09-16 19:34:33.708Z | 177.668° S |
| 4 mins | 2025-09-16 21:06:33.708Z | 317.816° NNW | 2025-09-16 21:08:33.708Z | 288.647° WNW | 16.316° | 2025-09-16 21:10:33.708Z | 262.7° W |
| 6 mins | 2025-09-17 06:40:33.708Z | 145.815° SSE | 2025-09-17 06:42:33.708Z | 92.519° ESE | 40.726° | 2025-09-17 06:46:33.708Z | 355.867° N |
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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