YUNYAO-1 47, 63348
Orbit data source: Space-Track
YUNYAO-1 47, 63348 is a payload satellite owned by Yunyao yuhang (CN) in SSO that was launched on Fri, 21 Mar 2025 UTC via a GUSHENXING 1 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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63348 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.6 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 YUNYAO-1 47
1 63348U 25059E 26008.98502081 .00004264 00000-0 26646-3 0 9997
2 63348 97.6007 191.3907 0016360 348.7478 11.3382 15.09892465 44265Epoch: 2026-01-08T23:38Z
TLE epoch observation values (Epoch: 2026-01-08T23:38:25.797Z)
Latitude
-0.00015°
Longitude
88.25196°
Altitude
528.506 km
Speed
7.605 km/s
True Right ascension
12h 45m 33s
True Declination
0° 00' 01"
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
05:16:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
544.823 km
Perigee altitude
522.209 km
Semi-major axis
6,911.653 km
Eccentricity
0.00164
Inclination
97.6007°
RAAN
191.3907°
Arg. of periapsis
348.7478°
True anomaly
11.37513°
Mean anomaly
11.3382°
Eccentric anomaly
11.35666°
Mean motion
3.7772 °/min
Orbital period
95.31 mins
BSTAR
0.00026646
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Other satellites on launch #59 in the year 2025 (2025-03-21 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 47 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 | 2026-01-09 12:30:02.916Z | 201.079° SSW | 2026-01-09 12:32:02.916Z | 251.827° W | 32.714° | 2026-01-09 12:35:02.916Z | 327.108° NNW |
| 4 mins | 2026-01-10 00:06:02.916Z | 68.935° E | 2026-01-10 00:07:02.916Z | 89.932° E | 19.925° | 2026-01-10 00:10:02.916Z | 143.359° SSE |
| 4 mins | 2026-01-10 01:40:02.916Z | 326.799° NNW | 2026-01-10 01:42:02.916Z | 279.947° WNW | 23.064° | 2026-01-10 01:44:02.916Z | 242.126° WSW |
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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