DECAYED

OBJECT Q, 57018 (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 Q, 57018 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
57018, 2023-085Q
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 Q
1 57018U 23085Q   25275.13397427  .11275987  25540-5  14073-2 0  9994
2 57018  97.4459  38.0354 0010990 268.0293  91.9745 16.35976847128476
Epoch: 2025-10-02T03:12Z
TLE epoch observation values (Epoch: 2025-10-02T03:12:55.376Z)
Latitude
-0.00011°
Longitude
-21.29432°
Altitude
180.027 km
Speed
7.798 km/s
True Right ascension
02h 32m 08s
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
21:29:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
180.542 km
Perigee altitude
166.141 km
Semi-major axis
6,551.478 km
Eccentricity
0.0011
Inclination
97.4459°
RAAN
38.0354°
Arg. of periapsis
268.0293°
True anomaly
92.10036°
Mean anomaly
91.9745°
Eccentric anomaly
92.03743°
Mean motion
4.09293 °/min
Orbital period
87.96 mins
BSTAR
0.0014073
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