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 spacecraft
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
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 YAOGAN-50
1 67433U 26006A 26065.23290774 .00000344 00000-0 14081-3 0 9998
2 67433 142.0348 78.2406 0001088 265.5415 94.5180 13.83249909 7179Epoch: 2026-03-06T05:35Z
TLE epoch observation values (Epoch: 2026-03-06T05:35:23.228Z)
Latitude
-0°
Longitude
-169.57803°
Altitude
951.716 km
Speed
7.378 km/s
True Right ascension
05h 12m 57s
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
03:03:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.783 km
Perigee altitude
954.187 km
Semi-major axis
7,333.122 km
Eccentricity
0.00011
Inclination
142.0348°
RAAN
78.2406°
Arg. of periapsis
265.5415°
True anomaly
94.53043°
Mean anomaly
94.518°
Eccentric anomaly
94.52421°
Mean motion
3.45629 °/min
Orbital period
104.16 mins
BSTAR
0.00014081
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-06 23:05:51.213Z | 166.11° S | 2026-03-06 23:08:51.213Z | 203.122° SW | 21.492° | 2026-03-06 23:12:51.213Z | 254.586° W |
| 9 mins | 2026-03-07 16:45:51.213Z | 96.506° ESE | 2026-03-07 16:49:51.213Z | 154.576° SSE | 30.863° | 2026-03-07 16:54:51.213Z | 221.046° SW |
| 9 mins | 2026-03-07 18:24:51.213Z | 91.67° ESE | 2026-03-07 18:28:51.213Z | 180.013° SSW | 42.393° | 2026-03-07 18:33:51.213Z | 250.897° W |
| 10 mins | 2026-03-07 20:02:51.213Z | 100.022° ESE | 2026-03-07 20:06:51.213Z | 147.135° SSE | 43.394° | 2026-03-07 20:12:51.213Z | 269.014° W |
| 9 mins | 2026-03-07 21:41:51.213Z | 127.391° SE | 2026-03-07 21:45:51.213Z | 195.304° SSW | 38.087° | 2026-03-07 21:50:51.213Z | 271.236° WNW |
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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