DECAYED

OBJECT Z, 57027 (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 Z, 57027 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
57027, 2023-085Z
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: 8 months ago

TLE from 8 months ago
0 OBJECT Z
1 57027U 23085Z   25289.55330619  .14464732  25899-5  44815-3 0  9991
2 57027  97.4442  52.0905 0011459 274.9767  85.0226 16.44024818130652
Epoch: 2025-10-16T13:16Z
TLE epoch observation values (Epoch: 2025-10-16T13:16:45.654Z)
Latitude
-0.00006°
Longitude
-172.41109°
Altitude
157.732 km
Speed
7.812 km/s
True Right ascension
03h 28m 21s
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
21:34:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.405 km
Perigee altitude
144.439 km
Semi-major axis
6,530.059 km
Eccentricity
0.00115
Inclination
97.4442°
RAAN
52.0905°
Arg. of periapsis
274.9767°
True anomaly
85.15343°
Mean anomaly
85.0226°
Eccentric anomaly
85.08801°
Mean motion
4.11308 °/min
Orbital period
87.53 mins
BSTAR
0.00044815
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
|