YAOGAN-35 05C, 53763
Orbit data source: Space-Track
YAOGAN-35 05C, 53763 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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53763 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: 21 hours ago
TLE from 21 hours ago
0 YAOGAN-35 05C
1 53763U 22109D 26172.55900148 .00006837 00000-0 28022-3 0 9999
2 53763 34.9928 329.4757 0003480 306.0801 53.9591 15.23577565211047Epoch: 2026-06-21T13:24Z
TLE epoch observation values (Epoch: 2026-06-21T13:24:57.727Z)
Latitude
-0.00004°
Longitude
-141.52243°
Altitude
492.56 km
Speed
7.622 km/s
True Right ascension
21h 57m 54s
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
21:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.705 km
Perigee altitude
495.919 km
Semi-major axis
6,876.449 km
Eccentricity
0.00035
Inclination
34.9928°
RAAN
329.4757°
Arg. of periapsis
306.0801°
True anomaly
53.99135°
Mean anomaly
53.9591°
Eccentric anomaly
53.97523°
Mean motion
3.80625 °/min
Orbital period
94.58 mins
BSTAR
0.00028022
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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 05C 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 14:51:38.022Z | 210.443° SW | 2026-06-22 14:53:38.022Z | 163.067° S | 25.012° | 2026-06-22 14:56:38.022Z | 107.838° ESE |
| 5 mins | 2026-06-22 16:30:38.022Z | 240.783° WSW | 2026-06-22 16:32:38.022Z | 194.345° SSW | 31.617° | 2026-06-22 16:35:38.022Z | 117.756° SE |
| 4 mins | 2026-06-22 18:10:38.022Z | 235.174° WSW | 2026-06-22 18:12:38.022Z | 188.239° SSW | 23.064° | 2026-06-22 18:14:38.022Z | 148.61° 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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