DECAYED

OBJECT E, 57008 (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 E, 57008 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
57008, 2023-085E
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: 5 months ago

TLE from 5 months ago
0 OBJECT E
1 57008U 23085E   26027.28316359  .08885833  25048-5  13813-2 0  9997
2 57008  97.4485 154.8921 0008178 295.9864  64.0589 16.33973218146316
Epoch: 2026-01-27T06:47Z
TLE epoch observation values (Epoch: 2026-01-27T06:47:45.334Z)
Latitude
-0.00003°
Longitude
-73.61358°
Altitude
182.782 km
Speed
7.798 km/s
True Right ascension
10h 19m 34s
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
21:27:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
184.064 km
Perigee altitude
173.339 km
Semi-major axis
6,556.838 km
Eccentricity
0.00082
Inclination
97.4485°
RAAN
154.8921°
Arg. of periapsis
295.9864°
True anomaly
64.14321°
Mean anomaly
64.0589°
Eccentric anomaly
64.10105°
Mean motion
4.08791 °/min
Orbital period
88.06 mins
BSTAR
0.0013813
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