CZ-2D R/B, 43486
Orbit data source: Space-Track
CZ-2D R/B, 43486 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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43486 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: 5 hours ago
TLE from 5 hours ago
0 CZ-2D R/B
1 43486U 18048C 25351.33002190 .00003056 00000-0 29283-3 0 9991
2 43486 97.5971 22.0449 0012719 53.1495 307.0889 14.93810099407991Epoch: 2025-12-17T07:55Z
TLE epoch observation values (Epoch: 2025-12-17T07:55:13.892Z)
Latitude
-0.00007°
Longitude
177.03559°
Altitude
583.782 km
Speed
7.571 km/s
True Right ascension
01h 28m 10s
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
11:13:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.932 km
Perigee altitude
574.224 km
Semi-major axis
6,961.215 km
Eccentricity
0.00127
Inclination
97.5971°
RAAN
22.0449°
Arg. of periapsis
53.1495°
True anomaly
306.97252°
Mean anomaly
307.0889°
Eccentric anomaly
307.03072°
Mean motion
3.73694 °/min
Orbital period
96.34 mins
BSTAR
0.00029283
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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 R/B 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-17 14:55:13.894Z | 19.903° NNE | 2025-12-17 14:58:13.894Z | 75.358° E | 42.043° | 2025-12-17 15:02:13.894Z | 183.423° SSW |
| 6 mins | 2025-12-18 01:44:13.894Z | 136.732° SSE | 2025-12-18 01:47:13.894Z | 79.755° E | 31.361° | 2025-12-18 01:50:13.894Z | 10.942° NNE |
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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