Showing default

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.

Loading next visibility...
Identifier
67433, 2026-006A
Orbit
LEO
Country
Flag of CNCN / PRC
Related 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)
2026-01-13 (8 months ago)
Launch vehicle
CHANG ZHENG 6A
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
14.304 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 YAOGAN-50
1 67433U 26006A   26259.09014721  .00000314  00000-0  11337-3 0  9991
2 67433 142.0417 295.0721 0001012 290.2247  69.8363 13.83249989 34020
Epoch: 2026-09-16T02:09Z
TLE epoch observation values (Epoch: 2026-09-16T02:09:48.718Z)
Latitude
-0.00003°
Longitude
-92.42758°
Altitude
951.397 km
Speed
7.378 km/s
True Right ascension
19h 40m 17s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:00:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.728 km
Perigee altitude
954.244 km
Semi-major axis
7,333.123 km
Eccentricity
0.0001
Inclination
142.0417°
RAAN
295.0721°
Arg. of periapsis
290.2247°
True anomaly
69.84719°
Mean anomaly
69.8363°
Eccentric anomaly
69.84174°
Mean motion
3.45629 °/min
Orbital period
104.16 mins
BSTAR
0.00011337
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #6 in the year 2026 (2026-01-13 UTC)

Documentation

Showing up to 5 results
|