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: 4 hours ago
TLE from 4 hours ago
0 OBJECT A
1 60012U 24110A 25344.23601446 .00011217 00000-0 68952-3 0 9996
2 60012 97.5776 72.6117 0009468 176.0562 184.0744 15.10186631 83360Epoch: 2025-12-10T05:39Z
TLE epoch observation values (Epoch: 2025-12-10T05:39:51.649Z)
Latitude
0.00002°
Longitude
-91.56275°
Altitude
545.233 km
Speed
7.586 km/s
True Right ascension
04h 50m 26s
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
07:28:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.16 km
Perigee altitude
526.074 km
Semi-major axis
6,910.754 km
Eccentricity
0.00095
Inclination
97.5776°
RAAN
72.6117°
Arg. of periapsis
176.0562°
True anomaly
184.0667°
Mean anomaly
184.0744°
Eccentric anomaly
184.07055°
Mean motion
3.77794 °/min
Orbital period
95.29 mins
BSTAR
0.00068952
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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 | 2025-12-10 18:57:00.452Z | 11.777° NNE | 2025-12-10 19:00:00.452Z | 1.69° NNE | 44.778° | 2025-12-10 19:03:00.452Z | 193.793° SSW |
| 5 mins | 2025-12-11 05:40:00.452Z | 130.499° SE | 2025-12-11 05:42:00.452Z | 75.467° E | 33.036° | 2025-12-11 05:45:00.452Z | 7.104° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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