OBJECT A, 66175
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 A, 66175 is a satellite owned by Yaogan Zongti (CN) in SSO that was launched on Sun, 26 Oct 2025 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). 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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66175 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
GF-14, Unknown motor
Mass
~6,500 kg wet, ~5,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 OBJECT A
1 66175U 25242A 25301.10588829 .00014793 00000-0 55401-3 0 9994
2 66175 97.4398 13.2893 0010327 261.9781 98.0286 15.27335919 301Epoch: 2025-10-28T02:32Z
TLE epoch observation values (Epoch: 2025-10-28T02:32:28.748Z)
Latitude
-0.00004°
Longitude
-61.52863°
Altitude
487.876 km
Speed
7.621 km/s
True Right ascension
00h 53m 09s
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
15:44:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.821 km
Perigee altitude
473.654 km
Semi-major axis
6,858.875 km
Eccentricity
0.00103
Inclination
97.4398°
RAAN
13.2893°
Arg. of periapsis
261.9781°
True anomaly
98.14576°
Mean anomaly
98.0286°
Eccentric anomaly
98.08718°
Mean motion
3.82088 °/min
Orbital period
94.22 mins
BSTAR
0.00055401
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Other satellites on launch #242 in the year 2025 (2025-10-26 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 A 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-01 04:10:21.779Z | 114.451° SE | 2025-11-01 04:12:21.779Z | 78.33° E | 18.772° | 2025-11-01 04:15:21.779Z | 21.532° NNE |
| 4 mins | 2025-11-01 05:44:21.779Z | 226.99° WSW | 2025-11-01 05:46:21.779Z | 273.539° WNW | 20.738° | 2025-11-01 05:48:21.779Z | 312.054° NW |
| 4 mins | 2025-11-01 17:11:21.779Z | 53.948° ENE | 2025-11-01 17:13:21.779Z | 103.99° ESE | 23.311° | 2025-11-01 17:15:21.779Z | 146.371° SSE |
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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