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, 5.0 m
Radar Cross Section
14.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 YAOGAN-50 02
1 68196U 26051A 26270.08885732 .00000287 00000-0 90581-4 0 9996
2 68196 141.9920 99.7375 0000527 274.0815 85.9845 13.83258660 27111Epoch: 2026-09-27T02:07Z
TLE epoch observation values (Epoch: 2026-09-27T02:07:57.272Z)
Latitude
0.00002°
Longitude
61.86125°
Altitude
951.6 km
Speed
7.378 km/s
True Right ascension
06h 38m 56s
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
15:44:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.334 km
Perigee altitude
954.561 km
Semi-major axis
7,333.084 km
Eccentricity
0.00005
Inclination
141.992°
RAAN
99.7375°
Arg. of periapsis
274.0815°
True anomaly
85.99052°
Mean anomaly
85.9845°
Eccentric anomaly
85.98751°
Mean motion
3.45631 °/min
Orbital period
104.16 mins
BSTAR
0.000090581
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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 | 2026-09-28 03:00:52.488Z | 116.277° SE | 2026-09-28 03:03:52.488Z | 148.336° SSE | 13.572° | 2026-09-28 03:05:52.488Z | 169.836° S |
| 9 mins | 2026-09-28 04:38:52.488Z | 98.189° ESE | 2026-09-28 04:42:52.488Z | 161.41° S | 37.07° | 2026-09-28 04:47:52.488Z | 222.7° SW |
| 10 mins | 2026-09-28 06:16:52.488Z | 89.136° E | 2026-09-28 06:21:52.488Z | 197.975° SSW | 64.355° | 2026-09-28 06:26:52.488Z | 251.807° W |
| 9 mins | 2026-09-28 07:55:52.488Z | 100.132° ESE | 2026-09-28 07:59:52.488Z | 171.607° S | 75.196° | 2026-09-28 08:04:52.488Z | 268.46° W |
| 9 mins | 2026-09-28 09:34:52.488Z | 128.592° SE | 2026-09-28 09:38:52.488Z | 206.766° SW | 51.965° | 2026-09-28 09:43:52.488Z | 272.627° WNW |
| 7 mins | 2026-09-28 11:14:52.488Z | 173.209° S | 2026-09-28 11:17:52.488Z | 214.976° SW | 23.573° | 2026-09-28 11:21:52.488Z | 260.661° 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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