YAOGAN-35 02A, 52907
Orbit data source: Space-Track
YAOGAN-35 02A, 52907 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Thu, 23 Jun 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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52907 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: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-35 02A
1 52907U 22068A 26172.52152411 .00005487 00000-0 22096-3 0 9996
2 52907 34.9904 111.2207 0008989 119.2448 240.9166 15.24186006222558Epoch: 2026-06-21T12:30Z
TLE epoch observation values (Epoch: 2026-06-21T12:30:59.683Z)
Latitude
-0.00003°
Longitude
13.75138°
Altitude
495.142 km
Speed
7.618 km/s
True Right ascension
07h 24m 52s
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
21:29:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.664 km
Perigee altitude
490.305 km
Semi-major axis
6,874.621 km
Eccentricity
0.0009
Inclination
34.9904°
RAAN
111.2207°
Arg. of periapsis
119.2448°
True anomaly
240.82663°
Mean anomaly
240.9166°
Eccentric anomaly
240.87161°
Mean motion
3.80776 °/min
Orbital period
94.54 mins
BSTAR
0.00022096
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Other satellites on launch #68 in the year 2022 (2022-06-23 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 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 23:20:12.554Z | 202.128° SSW | 2026-06-22 23:22:12.554Z | 168.623° S | 17.769° | 2026-06-22 23:25:12.554Z | 114.885° SE |
| 5 mins | 2026-06-23 01:00:12.554Z | 223.418° SW | 2026-06-23 01:02:12.554Z | 162.133° S | 30.117° | 2026-06-23 01:05:12.554Z | 107.7° ESE |
| 5 mins | 2026-06-23 02:39:12.554Z | 241.972° WSW | 2026-06-23 02:41:12.554Z | 192.493° SSW | 28.688° | 2026-06-23 02:44:12.554Z | 127.88° 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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