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, 5.0 m
Radar Cross Section
14.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-50
1 67433U 26006A 26256.92415031 .00000321 00000-0 11969-3 0 9998
2 67433 142.0416 284.6035 0001072 287.3170 72.7432 13.83249507 33721Epoch: 2026-09-13T22:10Z
TLE epoch observation values (Epoch: 2026-09-13T22:10:46.586Z)
Latitude
-0°
Longitude
-41.00243°
Altitude
951.421 km
Speed
7.378 km/s
True Right ascension
18h 58m 24s
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
20:39:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.773 km
Perigee altitude
954.201 km
Semi-major axis
7,333.124 km
Eccentricity
0.00011
Inclination
142.0416°
RAAN
284.6035°
Arg. of periapsis
287.317°
True anomaly
72.75493°
Mean anomaly
72.7432°
Eccentric anomaly
72.74907°
Mean motion
3.45629 °/min
Orbital period
104.16 mins
BSTAR
0.00011969
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-14 16:08:08.520Z | 119.211° SE | 2026-09-14 16:10:08.520Z | 140.443° SSE | 13.488° | 2026-09-14 16:13:08.520Z | 172.747° S |
| 8 mins | 2026-09-14 17:46:08.520Z | 100.706° ESE | 2026-09-14 17:49:08.520Z | 145.337° SSE | 36.467° | 2026-09-14 17:54:08.520Z | 219.115° SW |
| 9 mins | 2026-09-14 19:24:08.520Z | 90.143° ESE | 2026-09-14 19:28:08.520Z | 154.529° SSE | 66.117° | 2026-09-14 19:33:08.520Z | 250.269° W |
| 9 mins | 2026-09-14 21:03:08.520Z | 100.975° ESE | 2026-09-14 21:07:08.520Z | 203.861° SW | 74.219° | 2026-09-14 21:12:08.520Z | 268.74° W |
| 10 mins | 2026-09-14 22:41:08.520Z | 125.376° SE | 2026-09-14 22:45:08.520Z | 181.32° SSW | 50.925° | 2026-09-14 22:51:08.520Z | 273.438° WNW |
| 7 mins | 2026-09-15 00:21:08.520Z | 166.577° S | 2026-09-15 00:24:08.520Z | 204.189° SW | 23.466° | 2026-09-15 00:28:08.520Z | 255.325° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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