OBJECT C, 66177
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, 66177 is a satellite owned by Yaogan Zongti (CN) in SSO that was launched on Sun, 26 Oct 2025 UTC launched 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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66177 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 OBJECT C
1 66177U 25242C 25299.40367106 .00004293 00000-0 21434-3 0 9991
2 66177 97.6110 12.4552 0044551 134.5252 225.9635 15.17165482 38Epoch: 2025-10-26T09:41Z
TLE epoch observation values (Epoch: 2025-10-26T09:41:17.179Z)
Latitude
-0°
Longitude
-167.88674°
Altitude
538.913 km
Speed
7.581 km/s
True Right ascension
00h 49m 49s
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
15:52:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.084 km
Perigee altitude
480.697 km
Semi-major axis
6,889.528 km
Eccentricity
0.00446
Inclination
97.611°
RAAN
12.4552°
Arg. of periapsis
134.5252°
True anomaly
225.59791°
Mean anomaly
225.9635°
Eccentric anomaly
225.78056°
Mean motion
3.79541 °/min
Orbital period
94.85 mins
BSTAR
0.00021434
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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 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 | 2025-11-01 05:06:41.611Z | 171.996° S | 2025-11-01 05:09:41.611Z | 304.961° NW | 43.827° | 2025-11-01 05:12:41.611Z | 344.704° N |
| 5 mins | 2025-11-01 18:12:41.611Z | 354.373° N | 2025-11-01 18:14:41.611Z | 307.132° NW | 35.8° | 2025-11-01 18:17:41.611Z | 214.991° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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