OBJECT C, 62731

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, 62731 is a satellite owned by Yunyao yuhang (CN) in SSO that was launched on Mon, 20 Jan 2025 UTC via a GUSHENXING 1 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
62731, 2025-013C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Changguang WJ
Mission
Operational Commercial Weather
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2025-01-20 (8 months ago)
Launch vehicle
GUSHENXING 1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 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 62731U 25013C   25259.25793690  .00004494  00000-0  29221-3 0  9994
2 62731  97.6301  64.1333 0013988 227.2426 132.7626 15.08433794 35998
Epoch: 2025-09-16T06:11Z
TLE epoch observation values (Epoch: 2025-09-16T06:11:25.748Z)
Latitude
-0.00002°
Longitude
-24.17481°
Altitude
550.633 km
Speed
7.583 km/s
True Right ascension
04h 16m 31s
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
09:29:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.65 km
Perigee altitude
528.302 km
Semi-major axis
6,916.113 km
Eccentricity
0.0014
Inclination
97.6301°
RAAN
64.1333°
Arg. of periapsis
227.2426°
True anomaly
132.88014°
Mean anomaly
132.7626°
Eccentric anomaly
132.82138°
Mean motion
3.77355 °/min
Orbital period
95.4 mins
BSTAR
0.00029221
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 #13 in the year 2025 (2025-01-20 UTC)

Documentation

Showing up to 5 results
|