DECAYED

OBJECT H, 43669 (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 H, 43669 was a satellite owned by Changsha Tianyi (CN) 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
43669, 2018-083H
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changsha Tianyi
Mission
Decayed Commercial Communications
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: 1 year ago

TLE from 1 year ago
0 OBJECT H
1 43669U 18083H   24130.99921043  .13914420  25146-5  50688-3 0  9992
2 43669  97.2952 170.3552 0012886 250.8284 109.1623 16.43032312307806
Epoch: 2024-05-09T23:58Z
TLE epoch observation values (Epoch: 2024-05-09T23:58:51.781Z)
Latitude
0.00001°
Longitude
-57.64657°
Altitude
163.782 km
Speed
7.806 km/s
True Right ascension
11h 21m 25s
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
20:23:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.966 km
Perigee altitude
146.129 km
Semi-major axis
6,532.684 km
Eccentricity
0.00129
Inclination
97.2952°
RAAN
170.3552°
Arg. of periapsis
250.8284°
True anomaly
109.30171°
Mean anomaly
109.1623°
Eccentric anomaly
109.23201°
Mean motion
4.1106 °/min
Orbital period
87.58 mins
BSTAR
0.00050688
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