OBJECT D, 60748
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 D, 60748 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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60748 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
JTXZ
Mission
Operational Commercial Imaging
Bus & Motor
JTX, Unknown motor
Mass
~50 kg wet, ~50 kg dry
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: 2 days ago
TLE from 2 days ago
0 OBJECT D
1 60748U 24153D 25255.57304478 .00000927 00000-0 48393-4 0 9996
2 60748 97.6502 22.8860 0004927 100.5358 259.6431 15.18495880 57591Epoch: 2025-09-12T13:45Z
TLE epoch observation values (Epoch: 2025-09-12T13:45:11.069Z)
Latitude
0.00002°
Longitude
-175.22894°
Altitude
514.079 km
Speed
7.606 km/s
True Right ascension
01h 31m 32s
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
01:02:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.757 km
Perigee altitude
503.972 km
Semi-major axis
6,885.501 km
Eccentricity
0.00049
Inclination
97.6502°
RAAN
22.886°
Arg. of periapsis
100.5358°
True anomaly
259.58757°
Mean anomaly
259.6431°
Eccentric anomaly
259.61533°
Mean motion
3.79874 °/min
Orbital period
94.77 mins
BSTAR
0.000048393
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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 D 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 | 2025-09-14 08:34:12.831Z | 165.437° S | 2025-09-14 08:38:12.831Z | 357.236° N | 43.466° | 2025-09-14 08:41:12.831Z | 348.661° N |
| 5 mins | 2025-09-14 21:41:12.831Z | 355.626° N | 2025-09-14 21:43:12.831Z | 262.253° W | 40.65° | 2025-09-14 21:46:12.831Z | 205.548° SW |
| 5 mins | 2025-09-15 08:19:12.831Z | 142.478° SSE | 2025-09-15 08:21:12.831Z | 87.246° E | 37.522° | 2025-09-15 08:24:12.831Z | 1.968° 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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