Showing default

YUXING-3 06, 68199

Orbit data source: Space-Track

YUXING-3 06, 68199 is a Chinese payload satellite in SSO that was launched on Mon, 16 Mar 2026 UTC via a KUAIZHOU-11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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
68199, 2026-052B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
MOFANG
Mission
Operational Commercial Technology
Bus & Motor
YX3, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2026-03-16 (5 months ago)
Launch vehicle
KUAIZHOU-11
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.1 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 YUXING-3 06
1 68199U 26052B   26219.74990727  .00002942  00000-0  17830-3 0  9992
2 68199  97.5304 293.7448 0013938 128.9277 231.3197 15.11273867 21831
Epoch: 2026-08-07T17:59Z
TLE epoch observation values (Epoch: 2026-08-07T17:59:51.988Z)
Latitude
-0.00009°
Longitude
67.50707°
Altitude
541.418 km
Speed
7.588 km/s
True Right ascension
19h 34m 58s
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
13:25:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.924 km
Perigee altitude
519.669 km
Semi-major axis
6,907.434 km
Eccentricity
0.00139
Inclination
97.5304°
RAAN
293.7448°
Arg. of periapsis
128.9277°
True anomaly
231.19515°
Mean anomaly
231.3197°
Eccentric anomaly
231.25741°
Mean motion
3.78066 °/min
Orbital period
95.22 mins
BSTAR
0.0001783
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...

Documentation

Showing up to 5 results
|