YUNYAO-1 20, 58760
Orbit data source: Space-Track
YUNYAO-1 20, 58760 is a payload satellite owned by Yunyao yuhang (CN) in LEO that was launched on Thu, 11 Jan 2024 UTC via a YINLI-1 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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58760 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
YY-1, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 YUNYAO-1 20
1 58760U 24009C 26095.24769409 .00015352 00000-0 78245-3 0 9999
2 58760 49.9763 161.9717 0004497 352.7015 7.3871 15.16879593123618Epoch: 2026-04-05T05:56Z
TLE epoch observation values (Epoch: 2026-04-05T05:56:40.769Z)
Latitude
0°
Longitude
-120.75402°
Altitude
512.754 km
Speed
7.61 km/s
True Right ascension
10h 47m 53s
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
19:28:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.152 km
Perigee altitude
512.951 km
Semi-major axis
6,894.189 km
Eccentricity
0.00045
Inclination
49.9763°
RAAN
161.9717°
Arg. of periapsis
352.7015°
True anomaly
7.39373°
Mean anomaly
7.3871°
Eccentric anomaly
7.39041°
Mean motion
3.79156 °/min
Orbital period
94.95 mins
BSTAR
0.00078245
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Other satellites on launch #9 in the year 2024 (2024-01-11 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.YUNYAO-1 20 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-05 14:21:33.148Z | 291.516° WNW | 2026-04-05 14:24:33.148Z | 236.838° WSW | 34.555° | 2026-04-05 14:28:33.148Z | 148.31° SSE |
| 5 mins | 2026-04-06 07:27:33.148Z | 237.295° WSW | 2026-04-06 07:29:33.148Z | 11.141° NNE | 44.904° | 2026-04-06 07:32:33.148Z | 54.907° ENE |
| 4 mins | 2026-04-06 09:07:33.148Z | 311.422° NW | 2026-04-06 09:08:33.148Z | 333.349° NNW | 22.123° | 2026-04-06 09:11:33.148Z | 33.755° NE |
| 4 mins | 2026-04-06 10:47:33.148Z | 335.965° NNW | 2026-04-06 10:48:33.148Z | 354.593° N | 17.73° | 2026-04-06 10:51:33.148Z | 47.903° ENE |
| 6 mins | 2026-04-06 12:26:33.148Z | 325.37° NNW | 2026-04-06 12:28:33.148Z | 10.289° NNE | 30.957° | 2026-04-06 12:32:33.148Z | 94.021° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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