OBJECT A, 52716

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 A, 52716 is a satellite owned by Changguang WJ (CN) in LEO that was launched on Fri, 20 May 2022 UTC via a CHANG ZHENG 2C/YZ-1S launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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
52716, 2022-056A
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changguang WJ
Mission
Non-operational Commercial Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
2022-05-20 (4 years ago)
Launch vehicle
CHANG ZHENG 2C/YZ-1S
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
2.320 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 OBJECT A
1 52716U 22056A   26172.56476407  .00000148  00000-0  81422-4 0  9997
2 52716  86.0034  21.7336 0020251  18.5145 341.6765 14.04404376209501
Epoch: 2026-06-21T13:33Z
TLE epoch observation values (Epoch: 2026-06-21T13:33:15.615Z)
Latitude
-0.00013°
Longitude
-91.34469°
Altitude
867.636 km
Speed
7.426 km/s
True Right ascension
01h 26m 56s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:55:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
890.288 km
Perigee altitude
860.909 km
Semi-major axis
7,253.735 km
Eccentricity
0.00203
Inclination
86.0034°
RAAN
21.7336°
Arg. of periapsis
18.5145°
True anomaly
341.60337°
Mean anomaly
341.6765°
Eccentric anomaly
341.63995°
Mean motion
3.51318 °/min
Orbital period
102.47 mins
BSTAR
0.000081422
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 #56 in the year 2022 (2022-05-20 UTC)

Documentation

Showing up to 5 results
|