OBJECT C, 60014
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, 60014 is a satellite owned by Tsinghua (CN) 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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60014 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Tsinghua
Mission
Operational Amateur Imaging
Bus & Motor
NAXING, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT C
1 60014U 24110C 25312.85779155 .00002730 00000-0 23976-3 0 9991
2 60014 97.5689 30.2323 0012043 162.1345 198.0303 14.97338338 68829Epoch: 2025-11-08T20:35Z
TLE epoch observation values (Epoch: 2025-11-08T20:35:13.189Z)
Latitude
-0.00006°
Longitude
33.14597°
Altitude
586.144 km
Speed
7.563 km/s
True Right ascension
02h 00m 55s
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
17:48:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.498 km
Perigee altitude
563.757 km
Semi-major axis
6,950.264 km
Eccentricity
0.0012
Inclination
97.5689°
RAAN
30.2323°
Arg. of periapsis
162.1345°
True anomaly
197.98765°
Mean anomaly
198.0303°
Eccentric anomaly
198.00897°
Mean motion
3.74577 °/min
Orbital period
96.11 mins
BSTAR
0.00023976
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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 C 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 | 2025-11-10 04:47:56.112Z | 135.183° SSE | 2025-11-10 04:50:56.112Z | 75.554° E | 31.008° | 2025-11-10 04:53:56.112Z | 10.631° NNE |
| 6 mins | 2025-11-10 18:04:56.112Z | 20.185° NNE | 2025-11-10 18:06:56.112Z | 84.155° E | 43.922° | 2025-11-10 18:10:56.112Z | 187.538° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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