DECAYED

OBJECT N, 53456 (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 N, 53456 was a Chinese satellite in LEO that was launched on Wed, 10 Aug 2022 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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
53456, 2022-098N
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changguang WJ
Mission
Decayed Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
2022-08-10 (3 years ago)
Launch vehicle
CHANG ZHENG 6
Launch site
Taiyaun Space Center, China (TSC)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 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 N
1 53456U 22098N   24236.20983798  .15928328  26471-5  30776-3 0  9996
2 53456  97.4993 350.8666 0015490 269.9120  90.0407 16.46066502113683
Epoch: 2024-08-23T05:02Z
TLE epoch observation values (Epoch: 2024-08-23T05:02:10.001Z)
Latitude
-0.00005°
Longitude
-56.66165°
Altitude
152.993 km
Speed
7.814 km/s
True Right ascension
23h 23m 27s
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
11:03:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.625 km
Perigee altitude
136.412 km
Semi-major axis
6,524.656 km
Eccentricity
0.00155
Inclination
97.4993°
RAAN
350.8666°
Arg. of periapsis
269.912°
True anomaly
90.2182°
Mean anomaly
90.0407°
Eccentric anomaly
90.12945°
Mean motion
4.11819 °/min
Orbital period
87.42 mins
BSTAR
0.00030776
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