YAOGAN-50 02, 68196
Orbit data source: Space-Track
YAOGAN-50 02, 68196 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Sun, 15 Mar 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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68196 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Radar Imaging
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
Box + 2 Pan, 2.3 m
Radar Cross Section
14.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 YAOGAN-50 02
1 68196U 26051A 26219.83804544 .00000293 00000-0 96006-4 0 9999
2 68196 141.9885 217.0415 0000869 264.8468 95.2153 13.83261078 20151Epoch: 2026-08-07T20:06Z
TLE epoch observation values (Epoch: 2026-08-07T20:06:47.126Z)
Latitude
0.00003°
Longitude
-41.0129°
Altitude
951.676 km
Speed
7.378 km/s
True Right ascension
14h 28m 09s
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
13:25:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.576 km
Perigee altitude
954.301 km
Semi-major axis
7,333.075 km
Eccentricity
0.00009
Inclination
141.9885°
RAAN
217.0415°
Arg. of periapsis
264.8468°
True anomaly
95.22522°
Mean anomaly
95.2153°
Eccentric anomaly
95.22026°
Mean motion
3.45632 °/min
Orbital period
104.16 mins
BSTAR
0.000096006
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Other satellites on launch #51 in the year 2026 (2026-03-15 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 02 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-08 14:04:05.962Z | 118.954° SE | 2026-08-08 14:06:05.962Z | 140.11° SSE | 13.032° | 2026-08-08 14:09:05.962Z | 172.421° S |
| 8 mins | 2026-08-08 15:42:05.962Z | 100.504° ESE | 2026-08-08 15:46:05.962Z | 167.693° S | 30.582° | 2026-08-08 15:50:05.962Z | 218.825° SW |
| 9 mins | 2026-08-08 17:20:05.962Z | 90.132° ESE | 2026-08-08 17:24:05.962Z | 152.315° SSE | 42.322° | 2026-08-08 17:29:05.962Z | 250.075° W |
| 9 mins | 2026-08-08 18:59:05.962Z | 101.014° ESE | 2026-08-08 19:03:05.962Z | 199.438° SSW | 43.912° | 2026-08-08 19:08:05.962Z | 268.593° W |
| 10 mins | 2026-08-08 20:37:05.962Z | 125.309° SE | 2026-08-08 20:41:05.962Z | 179.751° S | 37.612° | 2026-08-08 20:47:05.962Z | 273.226° WNW |
| 7 mins | 2026-08-08 22:17:05.962Z | 166.22° S | 2026-08-08 22:20:05.962Z | 203.396° SW | 21.561° | 2026-08-08 22:24:05.962Z | 254.827° 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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