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 spacecraft
Bus & Motor
NAXING, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT C
1 60014U 24110C 25260.99458344 .00001114 00000-0 10162-3 0 9990
2 60014 97.5731 340.0014 0011644 351.0718 9.0295 14.97014395 61069Epoch: 2025-09-17T23:52Z
TLE epoch observation values (Epoch: 2025-09-17T23:52:12.009Z)
Latitude
-0.00003°
Longitude
-15.21118°
Altitude
571.183 km
Speed
7.58 km/s
True Right ascension
22h 40m 00s
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
22:40:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.225 km
Perigee altitude
565.037 km
Semi-major axis
6,951.268 km
Eccentricity
0.00116
Inclination
97.5731°
RAAN
340.0014°
Arg. of periapsis
351.0718°
True anomaly
9.05047°
Mean anomaly
9.0295°
Eccentric anomaly
9.03998°
Mean motion
3.74496 °/min
Orbital period
96.13 mins
BSTAR
0.00010162
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 06:25:23.713Z | 232.115° WSW | 2025-09-18 06:27:23.713Z | 264.896° W | 16.192° | 2025-09-18 06:29:23.713Z | 298.783° NW |
| 7 mins | 2025-09-18 18:05:23.713Z | 19.337° NNE | 2025-09-18 18:08:23.713Z | 106.151° ESE | 43.31° | 2025-09-18 18:12:23.713Z | 185.747° SSW |
| 6 mins | 2025-09-19 04:53:23.713Z | 130.946° SE | 2025-09-19 04:55:23.713Z | 89.607° E | 30.738° | 2025-09-19 04:59:23.713Z | 5.587° NNE |
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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