YAOGAN-50, 67433
Orbit data source: Space-Track
YAOGAN-50, 67433 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Tue, 13 Jan 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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67433 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Radar Imaging
Bus & Motor
YG50, Unknown motor
Mass
~1,500 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.2 m
Radar Cross Section
14.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-50
1 67433U 26006A 26171.36700001 .00000330 00000-0 12791-3 0 9990
2 67433 142.0358 231.1277 0001003 267.5008 92.5596 13.83250911 21870Epoch: 2026-06-20T08:48Z
TLE epoch observation values (Epoch: 2026-06-20T08:48:28.800Z)
Latitude
-0.00004°
Longitude
-169.5749°
Altitude
951.682 km
Speed
7.378 km/s
True Right ascension
15h 24m 30s
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
07:18:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.717 km
Perigee altitude
954.246 km
Semi-major axis
7,333.118 km
Eccentricity
0.0001
Inclination
142.0358°
RAAN
231.1277°
Arg. of periapsis
267.5008°
True anomaly
92.57108°
Mean anomaly
92.5596°
Eccentric anomaly
92.56534°
Mean motion
3.45629 °/min
Orbital period
104.16 mins
BSTAR
0.00012791
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Other satellites on launch #6 in the year 2026 (2026-01-13 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-50 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-20 21:21:02.898Z | 88.07° E | 2026-06-20 21:26:02.898Z | 157.679° S | 42.369° | 2026-06-20 21:31:02.898Z | 250.131° W |
| 9 mins | 2026-06-20 23:01:02.898Z | 101.387° ESE | 2026-06-20 23:05:02.898Z | 206.75° SW | 43.759° | 2026-06-20 23:10:02.898Z | 268.563° W |
| 9 mins | 2026-06-21 00:39:02.898Z | 125.772° SE | 2026-06-21 00:43:02.898Z | 182.734° SSW | 37.707° | 2026-06-21 00:48:02.898Z | 269.902° W |
| 7 mins | 2026-06-21 02:19:02.898Z | 167.01° S | 2026-06-21 02:22:02.898Z | 204.697° SW | 21.559° | 2026-06-21 02:26:02.898Z | 255.435° W |
| 9 mins | 2026-06-21 19:59:02.898Z | 97.203° ESE | 2026-06-21 20:03:02.898Z | 156.977° SSE | 30.866° | 2026-06-21 20:08:02.898Z | 221.549° SW |
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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