CZ-2D DEB, 43490
Orbit data source: Space-Track
CZ-2D DEB, 43490 is space debris in SSO originally from a launch on Sat, 02 Jun 2018 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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43490 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 CZ-2D DEB
1 43490U 18048E 25258.36946994 .00007781 00000-0 76163-3 0 9992
2 43490 98.2450 46.7436 0024360 333.2053 26.7905 14.92384526393136Epoch: 2025-09-15T08:52Z
TLE epoch observation values (Epoch: 2025-09-15T08:52:02.202Z)
Latitude
-0°
Longitude
-80.84068°
Altitude
578.382 km
Speed
7.58 km/s
True Right ascension
03h 06m 58s
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
15:10:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.511 km
Perigee altitude
570.575 km
Semi-major axis
6,965.68 km
Eccentricity
0.00244
Inclination
98.245°
RAAN
46.7436°
Arg. of periapsis
333.2053°
True anomaly
26.91666°
Mean anomaly
26.7905°
Eccentric anomaly
26.85355°
Mean motion
3.73334 °/min
Orbital period
96.43 mins
BSTAR
0.00076163
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Other satellites on launch #48 in the year 2018 (2018-06-02 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 23:54:46.072Z | 335.386° NNW | 2025-09-15 23:57:46.072Z | 286.456° WNW | 18.244° | 2025-09-15 23:59:46.072Z | 254.715° W |
| 5 mins | 2025-09-16 09:09:46.072Z | 108.239° ESE | 2025-09-16 09:11:46.072Z | 69.175° E | 22.087° | 2025-09-16 09:14:46.072Z | 17.676° NNE |
| 5 mins | 2025-09-16 10:44:46.072Z | 216.696° SW | 2025-09-16 10:46:46.072Z | 253.586° W | 23.12° | 2025-09-16 10:49:46.072Z | 312.677° NW |
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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