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: 10 hours ago
TLE from 10 hours ago
0 OBJECT C
1 60014U 24110C 25299.49202574 .00002914 00000-0 25621-3 0 9994
2 60014 97.5684 17.2868 0011327 207.2549 152.8080 14.97252886 66825Epoch: 2025-10-26T11:48Z
TLE epoch observation values (Epoch: 2025-10-26T11:48:31.023Z)
Latitude
-0.00007°
Longitude
165.0501°
Altitude
585.453 km
Speed
7.564 km/s
True Right ascension
01h 09m 08s
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
17:02:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.265 km
Perigee altitude
564.519 km
Semi-major axis
6,950.529 km
Eccentricity
0.00113
Inclination
97.5684°
RAAN
17.2868°
Arg. of periapsis
207.2549°
True anomaly
152.86724°
Mean anomaly
152.808°
Eccentric anomaly
152.83763°
Mean motion
3.74556 °/min
Orbital period
96.11 mins
BSTAR
0.00025621
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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 | 2025-10-27 05:35:31.983Z | 186.808° SSW | 2025-10-27 05:37:31.983Z | 242.953° WSW | 40.77° | 2025-10-27 05:41:31.983Z | 339.742° N |
| 5 mins | 2025-10-27 18:51:31.983Z | 338.576° N | 2025-10-27 18:53:31.983Z | 296.887° NW | 26.511° | 2025-10-27 18:56:31.983Z | 234.321° WSW |
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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