YAOGAN-35 05B, 53761
Orbit data source: Space-Track
YAOGAN-35 05B, 53761 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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53761 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 05B
1 53761U 22109B 25355.28692253 .00013097 00000-0 41990-3 0 9999
2 53761 34.9811 9.1803 0005394 337.0082 23.0393 15.31503742183514Epoch: 2025-12-21T06:53Z
TLE epoch observation values (Epoch: 2025-12-21T06:53:10.106Z)
Latitude
-0.00002°
Longitude
175.78662°
Altitude
466.827 km
Speed
7.637 km/s
True Right ascension
00h 36m 43s
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
13:57:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.287 km
Perigee altitude
470.894 km
Semi-major axis
6,852.727 km
Eccentricity
0.00054
Inclination
34.9811°
RAAN
9.1803°
Arg. of periapsis
337.0082°
True anomaly
23.06351°
Mean anomaly
23.0393°
Eccentric anomaly
23.0514°
Mean motion
3.82603 °/min
Orbital period
94.09 mins
BSTAR
0.0004199
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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 05B 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 05:02:07.972Z | 208.297° SW | 2025-12-22 05:04:07.972Z | 173.25° S | 19.304° | 2025-12-22 05:07:07.972Z | 114.512° SE |
| 5 mins | 2025-12-22 06:41:07.972Z | 235.325° WSW | 2025-12-22 06:43:07.972Z | 188.476° SSW | 30.365° | 2025-12-22 06:46:07.972Z | 113.43° SE |
| 5 mins | 2025-12-22 08:20:07.972Z | 243.229° WSW | 2025-12-22 08:22:07.972Z | 197.706° SSW | 26.328° | 2025-12-22 08:25:07.972Z | 133.06° 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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