CZ-2D DEB, 43102 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 43102 was space debris in LEO originally from a launch on Tue, 09 Jan 2018 UTC launched from the Taiyaun Space Center, China (TSC). 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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43102 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 year ago
Origin
Manufacturer
CALT
Mission
Decayed 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 & history
TLE from 1 year ago
0 CZ-2D DEB
1 43102U 18002D 24148.35516563 .10049319 23860-5 11920-2 0 9990
2 43102 97.1521 178.6641 0012999 245.2579 114.7367 16.36358875353163Epoch: 2024-05-27T08:31Z
TLE epoch observation values (Epoch: 2024-05-27T08:31:26.31Z)
Latitude
-0°
Longitude
165.41161°
Altitude
182.335 km
Speed
7.795 km/s
True Right ascension
11h 54m 39s
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
19:36:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
180.823 km
Perigee altitude
163.793 km
Semi-major axis
6,550.445 km
Eccentricity
0.0013
Inclination
97.1521°
RAAN
178.6641°
Arg. of periapsis
245.2579°
True anomaly
114.8719°
Mean anomaly
114.7367°
Eccentric anomaly
114.80431°
Mean motion
4.0939 °/min
Orbital period
87.94 mins
BSTAR
0.001192
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Other satellites on launch #2 in the year 2018 (2018-01-09 UTC)
CZ-2D DEB Visibility
Observer location: undefined°, undefined°
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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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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