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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-35 05C
1 53763U 22109D 25355.28159416 .00007276 00000-0 32876-3 0 9995
2 53763 34.9929 34.3020 0003132 130.5146 229.5841 15.20256044183252Epoch: 2025-12-21T06:45Z
TLE epoch observation values (Epoch: 2025-12-21T06:45:29.735Z)
Latitude
-0°
Longitude
-157.16819°
Altitude
505.373 km
Speed
7.613 km/s
True Right ascension
02h 17m 12s
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
13:57:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.472 km
Perigee altitude
506.158 km
Semi-major axis
6,886.452 km
Eccentricity
0.00031
Inclination
34.9929°
RAAN
34.302°
Arg. of periapsis
130.5146°
True anomaly
229.55678°
Mean anomaly
229.5841°
Eccentric anomaly
229.57044°
Mean motion
3.79796 °/min
Orbital period
94.79 mins
BSTAR
0.00032876
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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 | 2025-12-22 06:38:45.428Z | 208.016° SW | 2025-12-22 06:41:45.428Z | 150.38° SSE | 20.311° | 2025-12-22 06:43:45.428Z | 115.431° SE |
| 5 mins | 2025-12-22 08:18:45.428Z | 232.796° WSW | 2025-12-22 08:20:45.428Z | 180.896° SSW | 31.741° | 2025-12-22 08:23:45.428Z | 111.941° ESE |
| 5 mins | 2025-12-22 09:58:45.428Z | 237.191° WSW | 2025-12-22 10:00:45.428Z | 184.018° SSW | 27.478° | 2025-12-22 10:03:45.428Z | 129.633° SE |
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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