YAOGAN-36 02B, 54043
Orbit data source: Space-Track
YAOGAN-36 02B, 54043 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Fri, 14 Oct 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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54043 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: 23 hours ago
TLE from 23 hours ago
0 YAOGAN-36 02B
1 54043U 22133B 26172.46441321 .00010276 00000-0 31905-3 0 9997
2 54043 34.9963 82.9838 0002319 148.8132 211.2724 15.32577502205500Epoch: 2026-06-21T11:08Z
TLE epoch observation values (Epoch: 2026-06-21T11:08:45.301Z)
Latitude
0.00002°
Longitude
6.13077°
Altitude
468.384 km
Speed
7.634 km/s
True Right ascension
05h 31m 56s
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
21:28:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.978 km
Perigee altitude
469.801 km
Semi-major axis
6,849.527 km
Eccentricity
0.00023
Inclination
34.9963°
RAAN
82.9838°
Arg. of periapsis
148.8132°
True anomaly
211.25861°
Mean anomaly
211.2724°
Eccentric anomaly
211.2655°
Mean motion
3.82871 °/min
Orbital period
94.03 mins
BSTAR
0.00031905
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Other satellites on launch #133 in the year 2022 (2022-10-14 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 02B 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 21:47:45.141Z | 205.06° SW | 2026-06-22 21:49:45.141Z | 165.196° S | 20.219° | 2026-06-22 21:51:45.141Z | 122.646° SE |
| 5 mins | 2026-06-22 23:26:45.141Z | 230.799° WSW | 2026-06-22 23:28:45.141Z | 171.451° S | 30.751° | 2026-06-22 23:31:45.141Z | 110.506° ESE |
| 4 mins | 2026-06-23 01:05:45.141Z | 235.819° WSW | 2026-06-23 01:07:45.141Z | 181.774° SSW | 25.519° | 2026-06-23 01:09:45.141Z | 139.173° 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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