YAOGAN-36 03A, 54372
Orbit data source: Space-Track
YAOGAN-36 03A, 54372 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Sun, 27 Nov 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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54372 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-36 03A
1 54372U 22160A 26172.54646295 .00016221 00000-0 46823-3 0 9999
2 54372 35.0006 295.0952 0002796 340.2580 19.8030 15.34803712198884Epoch: 2026-06-21T13:06Z
TLE epoch observation values (Epoch: 2026-06-21T13:06:54.398Z)
Latitude
-0.00002°
Longitude
-171.37667°
Altitude
458.606 km
Speed
7.641 km/s
True Right ascension
19h 40m 22s
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
21:33:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.684 km
Perigee altitude
462.857 km
Semi-major axis
6,842.907 km
Eccentricity
0.00028
Inclination
35.0006°
RAAN
295.0952°
Arg. of periapsis
340.258°
True anomaly
19.81386°
Mean anomaly
19.803°
Eccentric anomaly
19.80843°
Mean motion
3.83427 °/min
Orbital period
93.89 mins
BSTAR
0.00046823
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Other satellites on launch #160 in the year 2022 (2022-11-27 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-36 03A 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 12:49:48.510Z | 207.251° SW | 2026-06-22 12:50:48.510Z | 182.131° SSW | 24.849° | 2026-06-22 12:53:48.510Z | 112.474° ESE |
| 5 mins | 2026-06-22 14:27:48.510Z | 240.167° WSW | 2026-06-22 14:29:48.510Z | 187.603° SSW | 30.629° | 2026-06-22 14:32:48.510Z | 118.149° SE |
| 4 mins | 2026-06-22 16:06:48.510Z | 234.883° WSW | 2026-06-22 16:08:48.510Z | 190.411° SSW | 20.062° | 2026-06-22 16:10:48.510Z | 152.283° 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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