YAOGAN-30 W, 46809
Orbit data source: Space-Track
YAOGAN-30 W, 46809 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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46809 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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 W
1 46809U 20076C 25311.32620302 .00005234 00000-0 40184-3 0 9996
2 46809 34.9973 1.6669 0006620 284.0933 75.9039 15.01172812274762Epoch: 2025-11-07T07:49Z
TLE epoch observation values (Epoch: 2025-11-07T07:49:43.940Z)
Latitude
-0.00003°
Longitude
-162.538°
Altitude
561.08 km
Speed
7.584 km/s
True Right ascension
00h 06m 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
13:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.095 km
Perigee altitude
561.901 km
Semi-major axis
6,944.635 km
Eccentricity
0.00066
Inclination
34.9973°
RAAN
1.6669°
Arg. of periapsis
284.0933°
True anomaly
75.97749°
Mean anomaly
75.9039°
Eccentric anomaly
75.94069°
Mean motion
3.75033 °/min
Orbital period
95.99 mins
BSTAR
0.00040184
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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 W 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-08 06:23:01.040Z | 183.65° SSW | 2025-11-08 06:25:01.040Z | 155.228° SSE | 13.44° | 2025-11-08 06:27:01.040Z | 125.843° SE |
| 5 mins | 2025-11-08 08:04:01.040Z | 212.267° SW | 2025-11-08 08:06:01.040Z | 162.856° S | 28.524° | 2025-11-08 08:09:01.040Z | 107.757° ESE |
| 6 mins | 2025-11-08 09:44:01.040Z | 246.651° WSW | 2025-11-08 09:47:01.040Z | 176.65° S | 33.779° | 2025-11-08 09:50:01.040Z | 116.522° SE |
| 5 mins | 2025-11-08 11:26:01.040Z | 235.457° WSW | 2025-11-08 11:28:01.040Z | 192.632° SSW | 23.786° | 2025-11-08 11:31:01.040Z | 143.59° SSE |
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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