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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 YAOGAN-30 U
1 46807U 20076A 25311.30353370 .00004967 00000-0 38249-3 0 9991
2 46807 34.9955 2.1870 0000779 235.1263 124.9372 15.01087915274733Epoch: 2025-11-07T07:17Z
TLE epoch observation values (Epoch: 2025-11-07T07:17:05.311Z)
Latitude
0°
Longitude
-153.83455°
Altitude
562.767 km
Speed
7.582 km/s
True Right ascension
00h 08m 44s
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
13:33:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.301 km
Perigee altitude
566.219 km
Semi-major axis
6,944.897 km
Eccentricity
0.00008
Inclination
34.9955°
RAAN
2.187°
Arg. of periapsis
235.1263°
True anomaly
124.94452°
Mean anomaly
124.9372°
Eccentric anomaly
124.94086°
Mean motion
3.75011 °/min
Orbital period
96 mins
BSTAR
0.00038249
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 07:28:36.497Z | 212.998° SW | 2025-11-08 07:31:36.497Z | 159.465° S | 23.452° | 2025-11-08 07:34:36.497Z | 109.005° ESE |
| 6 mins | 2025-11-08 09:09:36.497Z | 240.839° WSW | 2025-11-08 09:12:36.497Z | 170.087° S | 33.597° | 2025-11-08 09:15:36.497Z | 110.854° ESE |
| 5 mins | 2025-11-08 10:51:36.497Z | 237.469° WSW | 2025-11-08 10:53:36.497Z | 187.163° SSW | 28.626° | 2025-11-08 10:56:36.497Z | 132.557° SE |
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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