OBJECT A, 60012
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, 60012 is a Chinese 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). 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.
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60012 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL1GF4, Unknown motor
Mass
~112 kg wet, ~112 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.5 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT A
1 60012U 24110A 25297.75365244 .00013667 00000-0 73323-3 0 9992
2 60012 97.5792 26.5520 0013535 167.0033 193.1550 15.14996670 76349Epoch: 2025-10-24T18:05Z
TLE epoch observation values (Epoch: 2025-10-24T18:05:15.570Z)
Latitude
-0.00008°
Longitude
81.84311°
Altitude
533.163 km
Speed
7.591 km/s
True Right ascension
01h 46m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:11:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.303 km
Perigee altitude
508.635 km
Semi-major axis
6,896.106 km
Eccentricity
0.00135
Inclination
97.5792°
RAAN
26.552°
Arg. of periapsis
167.0033°
True anomaly
193.11976°
Mean anomaly
193.155°
Eccentric anomaly
193.13737°
Mean motion
3.78998 °/min
Orbital period
94.99 mins
BSTAR
0.00073323
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Other satellites on launch #110 in the year 2024 (2024-06-06 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-25 05:19:20.472Z | 123.507° SE | 2025-10-25 05:22:20.472Z | 69.467° E | 22.153° | 2025-10-25 05:25:20.472Z | 16.052° NNE |
| 5 mins | 2025-10-25 18:27:20.472Z | 48.634° ENE | 2025-10-25 18:29:20.472Z | 109.712° ESE | 29.661° | 2025-10-25 18:32:20.472Z | 164.847° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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