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OBJECT C, 62731

Orbit data source: Space-Track

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Recently launched and/or uncataloged RSOs may have evolving metadata. Metadata may include the following, but is not limited to: Owner, Manufacturer, Bus, Motor, and Mission.

OBJECT C, 62731 is a Chinese payload satellite 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
62731, 2025-013C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2025-01-20 (2 years ago)
Launch vehicle
GUSHENXING 1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
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: 8 hours ago

TLE from 8 hours ago
0 OBJECT C
1 62731U 25013C   26318.91652360  .00003430  00000-0  20265-3 0  9990
2 62731  97.6610 128.2907 0013080 210.9219 149.1242 15.12115993100107
Epoch: 2026-11-14T21:59Z
TLE epoch observation values (Epoch: 2026-11-14T21:59:47.639Z)
Latitude
-0.00002°
Longitude
104.32776°
Altitude
540.58 km
Speed
7.588 km/s
True Right ascension
08h 33m 09s
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
02:30:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.767 km
Perigee altitude
517.704 km
Semi-major axis
6,904.872 km
Eccentricity
0.00131
Inclination
97.661°
RAAN
128.2907°
Arg. of periapsis
210.9219°
True anomaly
149.20101°
Mean anomaly
149.1242°
Eccentric anomaly
149.16262°
Mean motion
3.78277 °/min
Orbital period
95.17 mins
BSTAR
0.00020265
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Other satellites on launch #13 in the year 2025 (2025-01-20 UTC)

Documentation

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