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.
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68199 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YUXING-3 06
1 68199U 26052B 26171.47564044 .00003763 00000-0 22967-3 0 9997
2 68199 97.5329 246.2070 0011057 300.8145 59.1996 15.10878363 14541Epoch: 2026-06-20T11:24Z
TLE epoch observation values (Epoch: 2026-06-20T11:24:55.334Z)
Latitude
-0°
Longitude
166.28672°
Altitude
532.686 km
Speed
7.599 km/s
True Right ascension
16h 24m 49s
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
10:19:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.142 km
Perigee altitude
522.865 km
Semi-major axis
6,908.64 km
Eccentricity
0.00111
Inclination
97.5329°
RAAN
246.207°
Arg. of periapsis
300.8145°
True anomaly
59.30851°
Mean anomaly
59.1996°
Eccentric anomaly
59.25405°
Mean motion
3.77967 °/min
Orbital period
95.25 mins
BSTAR
0.00022967
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Other satellites on launch #52 in the year 2026 (2026-03-16 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.YUXING-3 06 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:01:31.719Z | 166.274° S | 2026-06-21 05:04:31.719Z | 152.566° SSE | 44.874° | 2026-06-21 05:07:31.719Z | 348.273° N |
| 5 mins | 2026-06-21 18:11:31.719Z | 353.387° N | 2026-06-21 18:13:31.719Z | 297.526° NW | 38.217° | 2026-06-21 18:16:31.719Z | 213.132° SW |
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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