YAOGAN-30 U, 46807
Orbit data source: Space-Track
YAOGAN-30 U, 46807 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Mon, 26 Oct 2020 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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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46807 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Defense Sigint
Bus & Motor
Unknown
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YAOGAN-30 U
1 46807U 20076A 26172.16696896 .00001965 00000-0 14639-3 0 9996
2 46807 34.9946 66.9726 0000823 280.8745 79.1870 15.02710189308710Epoch: 2026-06-21T04:00Z
TLE epoch observation values (Epoch: 2026-06-21T04:00:26.118Z)
Latitude
-0.00004°
Longitude
97.49259°
Altitude
557.353 km
Speed
7.585 km/s
True Right ascension
04h 27m 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
21:38:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.337 km
Perigee altitude
561.194 km
Semi-major axis
6,939.903 km
Eccentricity
0.00008
Inclination
34.9946°
RAAN
66.9726°
Arg. of periapsis
280.8745°
True anomaly
79.19626°
Mean anomaly
79.187°
Eccentric anomaly
79.19163°
Mean motion
3.75416 °/min
Orbital period
95.89 mins
BSTAR
0.00014639
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Other satellites on launch #76 in the year 2020 (2020-10-26 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-30 U 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 | 2026-06-22 20:06:15.936Z | 193.765° SSW | 2026-06-22 20:08:15.936Z | 160.287° S | 18.248° | 2026-06-22 20:11:15.936Z | 113.011° SE |
| 6 mins | 2026-06-22 21:46:15.936Z | 233.723° WSW | 2026-06-22 21:49:15.936Z | 167.377° S | 31.678° | 2026-06-22 21:52:15.936Z | 108.486° ESE |
| 6 mins | 2026-06-22 23:27:15.936Z | 248.616° W | 2026-06-22 23:30:15.936Z | 179.232° S | 31.701° | 2026-06-22 23:33:15.936Z | 123.13° SE |
| 4 mins | 2026-06-23 01:09:15.936Z | 229.887° WSW | 2026-06-23 01:11:15.936Z | 192.615° SSW | 18.248° | 2026-06-23 01:13:15.936Z | 161.416° S |
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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