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OBJECT A, 60012

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 A, 60012 is a Chinese payload satellite in SSO that was launched on Thu, 06 Jun 2024 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
60012, 2024-110A
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL1GF4, Unknown motor
Mass
~112 kg wet, ~112 kg dry
Launch date (UTC)
2024-06-06 (2 years ago)
Launch vehicle
GUSHENXING 1
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.9 m
Radar Cross Section
1.500 m², Large (>1 m²)

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

TLE from 11 hours ago
0 OBJECT A
1 60012U 24110A   26308.54428528  .00004355  00000-0  27090-3 0  9992
2 60012  97.5673  38.8116 0025074  77.3969 283.0062 15.09883513133117
Epoch: 2026-11-04T13:03Z
TLE epoch observation values (Epoch: 2026-11-04T13:03:46.248Z)
Latitude
-0.00002°
Longitude
159.07783°
Altitude
535.766 km
Speed
7.597 km/s
True Right ascension
02h 35m 14s
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
19:48:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.872 km
Perigee altitude
516.212 km
Semi-major axis
6,911.679 km
Eccentricity
0.00251
Inclination
97.5673°
RAAN
38.8116°
Arg. of periapsis
77.3969°
True anomaly
282.72605°
Mean anomaly
283.0062°
Eccentric anomaly
282.86614°
Mean motion
3.77718 °/min
Orbital period
95.31 mins
BSTAR
0.0002709
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Other satellites on launch #110 in the year 2024 (2024-06-06 UTC)

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