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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-50
1 67433U 26006A 26048.84350002 .00000340 00000-0 13714-3 0 9995
2 67433 142.0343 359.0374 0000813 257.3639 102.6989 13.83245003 4907Epoch: 2026-02-17T20:14Z
TLE epoch observation values (Epoch: 2026-02-17T20:14:38.401Z)
Latitude
-0.00003°
Longitude
-92.44025°
Altitude
951.802 km
Speed
7.378 km/s
True Right ascension
23h 56m 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
06:13:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.598 km
Perigee altitude
954.406 km
Semi-major axis
7,333.139 km
Eccentricity
0.00008
Inclination
142.0343°
RAAN
359.0374°
Arg. of periapsis
257.3639°
True anomaly
102.70799°
Mean anomaly
102.6989°
Eccentric anomaly
102.70344°
Mean motion
3.45627 °/min
Orbital period
104.16 mins
BSTAR
0.00013714
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-18 10:44:04.910Z | 119.508° SE | 2026-02-18 10:46:04.910Z | 140.73° SSE | 13.007° | 2026-02-18 10:48:04.910Z | 163.013° S |
| 8 mins | 2026-02-18 12:22:04.910Z | 101.065° ESE | 2026-02-18 12:25:04.910Z | 145.851° SSE | 30.551° | 2026-02-18 12:30:04.910Z | 219.041° SW |
| 9 mins | 2026-02-18 14:00:04.910Z | 90.447° ESE | 2026-02-18 14:04:04.910Z | 155.688° SSE | 42.333° | 2026-02-18 14:09:04.910Z | 250.069° W |
| 9 mins | 2026-02-18 15:39:04.910Z | 101.309° ESE | 2026-02-18 15:43:04.910Z | 203.867° SW | 43.807° | 2026-02-18 15:48:04.910Z | 268.527° W |
| 9 mins | 2026-02-18 17:17:04.910Z | 125.636° SE | 2026-02-18 17:21:04.910Z | 181.589° SSW | 37.639° | 2026-02-18 17:26:04.910Z | 269.769° W |
| 7 mins | 2026-02-18 18:57:04.910Z | 166.717° S | 2026-02-18 19:00:04.910Z | 204.177° SW | 21.534° | 2026-02-18 19:04:04.910Z | 255.155° 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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