DECAYED

OBJECT D, 43665 (Decayed)

Orbit data source: Space-Track

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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT D, 43665 was a Chinese satellite in LEO that was launched on Mon, 29 Oct 2018 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
43665, 2018-083D
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Changsha Tianyi
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
2018-10-29 (7 years ago)
Launch vehicle
CHANG ZHENG 2C
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 OBJECT D
1 43665U 18083D   25001.57111115  .17470623  25571-5  41277-3 0  9993
2 43665  97.2770  41.4729 0010546 243.4715 116.5507 16.45549368343889
Epoch: 2025-01-01T13:42Z
TLE epoch observation values (Epoch: 2025-01-01T13:42:24.003Z)
Latitude
-0.00001°
Longitude
94.41041°
Altitude
157.429 km
Speed
7.81 km/s
True Right ascension
02h 45m 53s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:23:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
154.759 km
Perigee altitude
140.994 km
Semi-major axis
6,526.014 km
Eccentricity
0.00105
Inclination
97.277°
RAAN
41.4729°
Arg. of periapsis
243.4715°
True anomaly
116.65874°
Mean anomaly
116.5507°
Eccentric anomaly
116.60473°
Mean motion
4.11691 °/min
Orbital period
87.44 mins
BSTAR
0.00041277
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