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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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: 8 hours ago
TLE from 8 hours ago
0 YUNYAO-1 47
1 63348U 25059E 26171.53623352 .00002563 00000-0 15605-3 0 9997
2 63348 97.6095 352.9201 0016914 142.8112 217.4293 15.11207091 68801Epoch: 2026-06-20T12:52Z
TLE epoch observation values (Epoch: 2026-06-20T12:52:10.576Z)
Latitude
0.00001°
Longitude
-108.87342°
Altitude
544.881 km
Speed
7.585 km/s
True Right ascension
23h 31m 40s
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
07:23:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.188 km
Perigee altitude
517.82 km
Semi-major axis
6,907.641 km
Eccentricity
0.00169
Inclination
97.6095°
RAAN
352.9201°
Arg. of periapsis
142.8112°
True anomaly
217.3117°
Mean anomaly
217.4293°
Eccentric anomaly
217.37048°
Mean motion
3.78049 °/min
Orbital period
95.23 mins
BSTAR
0.00015605
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 00:34:10.387Z | 34.372° NE | 2026-06-21 00:37:10.387Z | 115.409° SE | 31.913° | 2026-06-21 00:40:10.387Z | 168.58° S |
| 4 mins | 2026-06-21 11:17:10.387Z | 96.074° ESE | 2026-06-21 11:18:10.387Z | 76.088° E | 18.752° | 2026-06-21 11:21:10.387Z | 22.573° NE |
| 4 mins | 2026-06-21 12:51:10.387Z | 226.464° WSW | 2026-06-21 12:53:10.387Z | 276.14° WNW | 23.557° | 2026-06-21 12:55:10.387Z | 314.285° NW |
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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