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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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 W
1 46809U 20076C 26172.38907991 .00002131 00000-0 15859-3 0 9994
2 46809 34.9965 65.2680 0005270 107.4651 252.6633 15.02697217308772Epoch: 2026-06-21T09:20Z
TLE epoch observation values (Epoch: 2026-06-21T09:20:16.504Z)
Latitude
-0.00004°
Longitude
15.60912°
Altitude
558.591 km
Speed
7.584 km/s
True Right ascension
04h 21m 04s
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
21:35:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.463 km
Perigee altitude
558.148 km
Semi-major axis
6,939.942 km
Eccentricity
0.00053
Inclination
34.9965°
RAAN
65.268°
Arg. of periapsis
107.4651°
True anomaly
252.60567°
Mean anomaly
252.6633°
Eccentric anomaly
252.63448°
Mean motion
3.75413 °/min
Orbital period
95.89 mins
BSTAR
0.00015859
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 20:40:01.849Z | 215.149° SW | 2026-06-22 20:43:01.849Z | 162.227° S | 23.783° | 2026-06-22 20:46:01.849Z | 109.621° ESE |
| 6 mins | 2026-06-22 22:21:01.849Z | 241.44° WSW | 2026-06-22 22:24:01.849Z | 169.837° S | 33.454° | 2026-06-22 22:27:01.849Z | 111.108° ESE |
| 6 mins | 2026-06-23 00:02:01.849Z | 248.242° W | 2026-06-23 00:05:01.849Z | 183.5° SSW | 27.731° | 2026-06-23 00:08:01.849Z | 132.452° 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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