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: 15 hours ago
TLE from 15 hours ago
0 YAOGAN-30 W
1 46809U 20076C 25300.81774942 .00004838 00000-0 37264-3 0 9992
2 46809 34.9958 65.5572 0006095 201.2620 158.7835 15.01074234273185Epoch: 2025-10-27T19:37Z
TLE epoch observation values (Epoch: 2025-10-27T19:37:33.549Z)
Latitude
-0.00003°
Longitude
94.75322°
Altitude
566.443 km
Speed
7.578 km/s
True Right ascension
04h 22m 13s
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
05:58:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.035 km
Perigee altitude
562.569 km
Semi-major axis
6,944.939 km
Eccentricity
0.00061
Inclination
34.9958°
RAAN
65.5572°
Arg. of periapsis
201.262°
True anomaly
158.80876°
Mean anomaly
158.7835°
Eccentric anomaly
158.79613°
Mean motion
3.75008 °/min
Orbital period
96 mins
BSTAR
0.00037264
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-28 11:48:40.366Z | 191.954° SSW | 2025-10-28 11:50:40.366Z | 161.32° S | 16.613° | 2025-10-28 11:53:40.366Z | 115.327° SE |
| 6 mins | 2025-10-28 13:29:40.366Z | 222.44° SW | 2025-10-28 13:31:40.366Z | 174.203° S | 30.862° | 2025-10-28 13:35:40.366Z | 103.293° ESE |
| 6 mins | 2025-10-28 15:10:40.366Z | 241.258° WSW | 2025-10-28 15:12:40.366Z | 190.859° SSW | 32.799° | 2025-10-28 15:16:40.366Z | 116.726° SE |
| 5 mins | 2025-10-28 16:51:40.366Z | 237.711° WSW | 2025-10-28 16:53:40.366Z | 200.983° SSW | 20.503° | 2025-10-28 16:56:40.366Z | 152.482° 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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