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 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, 2.3 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-50 02
1 68196U 26051A 26171.46434939 .00000299 00000-0 10136-3 0 9997
2 68196 141.9917 343.4220 0000574 260.4808 99.5847 13.83270130 13448Epoch: 2026-06-20T11:08Z
TLE epoch observation values (Epoch: 2026-06-20T11:08:39.787Z)
Latitude
0°
Longitude
-92.42238°
Altitude
951.656 km
Speed
7.378 km/s
True Right ascension
22h 53m 41s
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
10:19:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.328 km
Perigee altitude
954.486 km
Semi-major axis
7,333.044 km
Eccentricity
0.00006
Inclination
141.9917°
RAAN
343.422°
Arg. of periapsis
260.4808°
True anomaly
99.59119°
Mean anomaly
99.5847°
Eccentric anomaly
99.58794°
Mean motion
3.45634 °/min
Orbital period
104.16 mins
BSTAR
0.00010136
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 01:38:29.804Z | 123.433° SE | 2026-06-21 01:40:29.804Z | 145.319° SSE | 13.107° | 2026-06-21 01:42:29.804Z | 167.157° S |
| 9 mins | 2026-06-21 03:15:29.804Z | 96.558° ESE | 2026-06-21 03:19:29.804Z | 155.152° SSE | 30.931° | 2026-06-21 03:24:29.804Z | 221.23° SW |
| 9 mins | 2026-06-21 04:54:29.804Z | 91.589° ESE | 2026-06-21 04:58:29.804Z | 181.753° SSW | 42.422° | 2026-06-21 05:03:29.804Z | 251.048° W |
| 10 mins | 2026-06-21 06:32:29.804Z | 99.915° ESE | 2026-06-21 06:36:29.804Z | 148.315° SSE | 43.501° | 2026-06-21 06:42:29.804Z | 269.158° W |
| 9 mins | 2026-06-21 08:11:29.804Z | 127.389° SE | 2026-06-21 08:15:29.804Z | 196.277° SSW | 38.175° | 2026-06-21 08:20:29.804Z | 271.461° WNW |
| 7 mins | 2026-06-21 09:51:29.804Z | 170.468° S | 2026-06-21 09:54:29.804Z | 210.536° SW | 21.713° | 2026-06-21 09:58:29.804Z | 258.467° 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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