YAOGAN-35 05A, 53760
Orbit data source: Space-Track
YAOGAN-35 05A, 53760 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Tue, 06 Sep 2022 UTC via a CHANG ZHENG 2D launch vehicle from the Xichang Space Center, China (XSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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53760 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Defense Sigint
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
11.063 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-35 05A
1 53760U 22109A 26172.51694218 .00008495 00000-0 35352-3 0 9996
2 53760 35.0082 311.6904 0002563 356.3395 3.7301 15.23023274211271Epoch: 2026-06-21T12:24Z
TLE epoch observation values (Epoch: 2026-06-21T12:24:23.804Z)
Latitude
0°
Longitude
-144.12486°
Altitude
493.878 km
Speed
7.621 km/s
True Right ascension
20h 46m 45s
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
21:41:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.739 km
Perigee altitude
498.214 km
Semi-major axis
6,878.113 km
Eccentricity
0.00026
Inclination
35.0082°
RAAN
311.6904°
Arg. of periapsis
356.3395°
True anomaly
3.73201°
Mean anomaly
3.7301°
Eccentric anomaly
3.73106°
Mean motion
3.80486 °/min
Orbital period
94.62 mins
BSTAR
0.00035352
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Other satellites on launch #109 in the year 2022 (2022-09-06 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.YAOGAN-35 05A 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 | 2026-06-22 13:51:49.148Z | 219.181° SW | 2026-06-22 13:53:49.148Z | 176.125° S | 26.338° | 2026-06-22 13:56:49.148Z | 110.886° ESE |
| 5 mins | 2026-06-22 15:31:49.148Z | 234.597° WSW | 2026-06-22 15:33:49.148Z | 171.737° S | 31.579° | 2026-06-22 15:36:49.148Z | 115.491° SE |
| 4 mins | 2026-06-22 17:11:49.148Z | 224.355° SW | 2026-06-22 17:12:49.148Z | 201.194° SSW | 21.576° | 2026-06-22 17:15:49.148Z | 146.022° 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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