OBJECT F, 60750
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 F, 60750 is a Chinese satellite in SSO that was launched on Thu, 29 Aug 2024 UTC via a GUSHENXING 1 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT F
1 60750U 24153F 25342.27538075 .00018842 00000-0 88764-3 0 9995
2 60750 97.6506 110.0926 0006260 185.2481 174.8689 15.19548556 70745Epoch: 2025-12-08T06:36Z
TLE epoch observation values (Epoch: 2025-12-08T06:36:32.896Z)
Latitude
-0.00001°
Longitude
-66.32122°
Altitude
514.581 km
Speed
7.604 km/s
True Right ascension
07h 20m 22s
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
12:16:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.489 km
Perigee altitude
499.873 km
Semi-major axis
6,882.318 km
Eccentricity
0.00063
Inclination
97.6506°
RAAN
110.0926°
Arg. of periapsis
185.2481°
True anomaly
174.87531°
Mean anomaly
174.8689°
Eccentric anomaly
174.87211°
Mean motion
3.80138 °/min
Orbital period
94.7 mins
BSTAR
0.00088764
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Other satellites on launch #153 in the year 2024 (2024-08-29 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 F 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-08 21:23:13.511Z | 18.643° NNE | 2025-12-08 21:27:13.511Z | 136.702° SSE | 40.606° | 2025-12-08 21:30:13.511Z | 182.855° SSW |
| 4 mins | 2025-12-09 08:03:13.511Z | 110.762° ESE | 2025-12-09 08:05:13.511Z | 61.796° ENE | 23.415° | 2025-12-09 08:07:13.511Z | 21.462° NNE |
| 4 mins | 2025-12-09 09:37:13.511Z | 234.868° WSW | 2025-12-09 09:39:13.511Z | 275.61° WNW | 17.395° | 2025-12-09 09:41:13.511Z | 309.304° NW |
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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