YAOGAN-35 04C, 53526
Orbit data source: Space-Track
YAOGAN-35 04C, 53526 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Fri, 19 Aug 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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53526 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-35 04C
1 53526U 22100E 26172.12958902 .00006490 00000-0 28029-3 0 9993
2 53526 34.9962 51.2337 0007938 89.3616 270.8008 15.21800311213561Epoch: 2026-06-21T03:06Z
TLE epoch observation values (Epoch: 2026-06-21T03:06:36.491Z)
Latitude
0°
Longitude
95.24737°
Altitude
499.246 km
Speed
7.617 km/s
True Right ascension
03h 24m 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
23:09:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.122 km
Perigee altitude
498.197 km
Semi-major axis
6,881.796 km
Eccentricity
0.00079
Inclination
34.9962°
RAAN
51.2337°
Arg. of periapsis
89.3616°
True anomaly
270.70984°
Mean anomaly
270.8008°
Eccentric anomaly
270.75532°
Mean motion
3.80181 °/min
Orbital period
94.69 mins
BSTAR
0.00028029
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Other satellites on launch #100 in the year 2022 (2022-08-19 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 04C 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 20:21:00.018Z | 211.601° SW | 2026-06-22 20:23:00.018Z | 155.496° SSE | 26.923° | 2026-06-22 20:26:00.018Z | 105.487° ESE |
| 5 mins | 2026-06-22 22:00:00.018Z | 241.018° WSW | 2026-06-22 22:02:00.018Z | 189.953° SSW | 31.417° | 2026-06-22 22:05:00.018Z | 119.942° SE |
| 4 mins | 2026-06-22 23:40:00.018Z | 232.688° WSW | 2026-06-22 23:42:00.018Z | 189.476° SSW | 20.026° | 2026-06-22 23:44:00.018Z | 153.749° 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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