OBJECT C, 57426

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 C, 57426 is a Chinese satellite in SSO that was launched on Sun, 23 Jul 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.

Loading next visibility...
Identifier
57426, 2023-104C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Yinhe
Mission
Operational Commercial Imaging
Bus & Motor
AS, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2023-07-23 (2 years ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Taiyaun Space Center, China (TSC)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.363 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 OBJECT C
1 57426U 23104C   25259.62803916  .00013732  00000-0  56095-3 0  9996
2 57426  97.3006 325.4350 0003653 108.7564 251.4070 15.24489338120055
Epoch: 2025-09-16T15:04Z
TLE epoch observation values (Epoch: 2025-09-16T15:04:22.583Z)
Latitude
-0.00007°
Longitude
103.5253°
Altitude
496.22 km
Speed
7.616 km/s
True Right ascension
21h 41m 44s
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
18:24:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.783 km
Perigee altitude
486.766 km
Semi-major axis
6,867.412 km
Eccentricity
0.00037
Inclination
97.3006°
RAAN
325.435°
Arg. of periapsis
108.7564°
True anomaly
251.36733°
Mean anomaly
251.407°
Eccentric anomaly
251.38716°
Mean motion
3.81376 °/min
Orbital period
94.39 mins
BSTAR
0.00056095
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...
Other satellites on launch #104 in the year 2023 (2023-07-23 UTC)

Documentation

Showing up to 5 results
|