DECAYED

OBJECT N, 57016 (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 N, 57016 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
57016, 2023-085N
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 N
1 57016U 23085N   25281.21692404  .18692083  26286-5  38875-3 0  9993
2 57016  97.4622  44.6182 0013216 261.8433  98.1370 16.45926555129396
Epoch: 2025-10-08T05:12Z
TLE epoch observation values (Epoch: 2025-10-08T05:12:22.237Z)
Latitude
-0.00003°
Longitude
-50.56909°
Altitude
154.574 km
Speed
7.813 km/s
True Right ascension
02h 58m 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
21:24:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
155.511 km
Perigee altitude
138.264 km
Semi-major axis
6,525.024 km
Eccentricity
0.00132
Inclination
97.4622°
RAAN
44.6182°
Arg. of periapsis
261.8433°
True anomaly
98.28688°
Mean anomaly
98.137°
Eccentric anomaly
98.21195°
Mean motion
4.11784 °/min
Orbital period
87.42 mins
BSTAR
0.00038875
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