DECAYED

OBJECT L, 53454 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

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

OBJECT L, 53454 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
53454, 2022-098L
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 L
1 53454U 22098L   24223.07089029  .16090869  26592-5  19277-3 0  9997
2 53454  97.4977 338.1171 0016225 261.0277  98.9190 16.48933712111701
Epoch: 2024-08-10T01:42Z
TLE epoch observation values (Epoch: 2024-08-10T01:42:04.921Z)
Latitude
-0.00004°
Longitude
-6.43962°
Altitude
147.062 km
Speed
7.817 km/s
True Right ascension
22h 32m 28s
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
11:09:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
149.519 km
Perigee altitude
128.371 km
Semi-major axis
6,517.082 km
Eccentricity
0.00162
Inclination
97.4977°
RAAN
338.1171°
Arg. of periapsis
261.0277°
True anomaly
99.10262°
Mean anomaly
98.919°
Eccentric anomaly
99.01082°
Mean motion
4.12537 °/min
Orbital period
87.26 mins
BSTAR
0.00019277
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|