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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Edit Public Description
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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 YAOGAN-50
1 67433U 26006A 26016.17880840 .00000537 00000-0 12658-3 0 9998
2 67433 141.9984 200.7842 0164962 123.7171 237.9391 14.21837795 375Epoch: 2026-01-16T04:17Z
TLE epoch observation values (Epoch: 2026-01-16T04:17:29.045Z)
Latitude
-0.00004°
Longitude
20.79142°
Altitude
882.803 km
Speed
7.38 km/s
True Right ascension
13h 23m 08s
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
22:42:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
940.562 km
Perigee altitude
703.019 km
Semi-major axis
7,199.927 km
Eccentricity
0.0165
Inclination
141.9984°
RAAN
200.7842°
Arg. of periapsis
123.7171°
True anomaly
236.35463°
Mean anomaly
237.9391°
Eccentric anomaly
237.14512°
Mean motion
3.55264 °/min
Orbital period
101.33 mins
BSTAR
0.00012658
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Other satellites on launch #6 in the year 2026 (2026-01-13 UTC)
Did you know?
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 | 2026-01-20 04:52:44.350Z | 96.256° ESE | 2026-01-20 04:56:44.350Z | 158.398° S | 25.819° | 2026-01-20 04:59:44.350Z | 209.53° SW |
| 7 mins | 2026-01-20 06:29:44.350Z | 93.266° ESE | 2026-01-20 06:32:44.350Z | 152.86° SSE | 40.667° | 2026-01-20 06:36:44.350Z | 246.695° WSW |
| 8 mins | 2026-01-20 08:05:44.350Z | 100.662° ESE | 2026-01-20 08:08:44.350Z | 145.776° SSE | 42.919° | 2026-01-20 08:13:44.350Z | 267.354° W |
| 8 mins | 2026-01-20 09:41:44.350Z | 126.633° SE | 2026-01-20 09:44:44.350Z | 175.479° S | 36.843° | 2026-01-20 09:49:44.350Z | 270.582° WNW |
| 6 mins | 2026-01-20 11:18:44.350Z | 167.347° S | 2026-01-20 11:21:44.350Z | 211.237° SW | 21.547° | 2026-01-20 11:24:44.350Z | 252.851° W |
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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