DECAYED

OBJECT U, 57022 (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 U, 57022 was a Chinese satellite in LEO that was launched on Thu, 15 Jun 2023 UTC via a CHANG ZHENG 2D 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
57022, 2023-085U
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2023-06-15 (3 years ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Taiyaun Space Center, China (TSC)
Object type
Unknown
Shape & HBR
Box, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 OBJECT U
1 57022U 23085U   25274.91897418  .13054562  25857-5  11605-2 0  9994
2 57022  97.4658  38.5598 0012214 266.4692  93.5210 16.38963109128445
Epoch: 2025-10-01T22:03Z
TLE epoch observation values (Epoch: 2025-10-01T22:03:19.369Z)
Latitude
0.00003°
Longitude
56.84201°
Altitude
172.311 km
Speed
7.802 km/s
True Right ascension
02h 34m 14s
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
00:39:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
173.366 km
Perigee altitude
157.382 km
Semi-major axis
6,543.511 km
Eccentricity
0.00122
Inclination
97.4658°
RAAN
38.5598°
Arg. of periapsis
266.4692°
True anomaly
93.66068°
Mean anomaly
93.521°
Eccentric anomaly
93.59084°
Mean motion
4.10041 °/min
Orbital period
87.8 mins
BSTAR
0.0011605
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
|