YAOGAN-36 02A, 54042
Orbit data source: Space-Track
YAOGAN-36 02A, 54042 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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54042 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: 1 day ago
TLE from 1 day ago
0 YAOGAN-36 02A
1 54042U 22133A 26172.24628032 .00007053 00000-0 29183-3 0 9992
2 54042 35.0069 94.2584 0026352 240.6954 119.1126 15.22927529205372Epoch: 2026-06-21T05:54Z
TLE epoch observation values (Epoch: 2026-06-21T05:54:38.619Z)
Latitude
-0.00005°
Longitude
96.14811°
Altitude
504.772 km
Speed
7.609 km/s
True Right ascension
06h 17m 01s
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
21:31:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.391 km
Perigee altitude
482.139 km
Semi-major axis
6,878.402 km
Eccentricity
0.00264
Inclination
35.0069°
RAAN
94.2584°
Arg. of periapsis
240.6954°
True anomaly
119.376°
Mean anomaly
119.1126°
Eccentric anomaly
119.24434°
Mean motion
3.80463 °/min
Orbital period
94.62 mins
BSTAR
0.00029183
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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 02A 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 23:06:46.564Z | 213.48° SW | 2026-06-22 23:08:46.564Z | 162.188° S | 27.404° | 2026-06-22 23:11:46.564Z | 107.164° ESE |
| 6 mins | 2026-06-23 00:45:46.564Z | 242.4° WSW | 2026-06-23 00:47:46.564Z | 196.31° SSW | 31.9° | 2026-06-23 00:51:46.564Z | 113.717° SE |
| 4 mins | 2026-06-23 02:25:46.564Z | 235.143° WSW | 2026-06-23 02:27:46.564Z | 191.879° SSW | 21.658° | 2026-06-23 02:29:46.564Z | 153.781° 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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