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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-30 W
1 46809U 20076C 26018.00690385 .00002685 00000-0 20438-3 0 9991
2 46809 34.9969 285.6155 0006605 206.7173 153.3196 15.01717431285546Epoch: 2026-01-18T00:09Z
TLE epoch observation values (Epoch: 2026-01-18T00:09:56.492Z)
Latitude
0.00002°
Longitude
165.70648°
Altitude
564.612 km
Speed
7.579 km/s
True Right ascension
19h 02m 27s
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
08:07:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.406 km
Perigee altitude
560.235 km
Semi-major axis
6,942.958 km
Eccentricity
0.00066
Inclination
34.9969°
RAAN
285.6155°
Arg. of periapsis
206.7173°
True anomaly
153.35356°
Mean anomaly
153.3196°
Eccentric anomaly
153.33658°
Mean motion
3.75169 °/min
Orbital period
95.96 mins
BSTAR
0.00020438
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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 | 2026-01-18 21:08:19.069Z | 194.256° SSW | 2026-01-18 21:10:19.069Z | 162.018° S | 17.981° | 2026-01-18 21:13:19.069Z | 114.373° SE |
| 5 mins | 2026-01-18 22:49:19.069Z | 224.255° SW | 2026-01-18 22:51:19.069Z | 173.585° S | 31.673° | 2026-01-18 22:54:19.069Z | 109.761° ESE |
| 5 mins | 2026-01-19 00:30:19.069Z | 240.364° WSW | 2026-01-19 00:32:19.069Z | 188.244° SSW | 32.222° | 2026-01-19 00:35:19.069Z | 124.338° SE |
| 4 mins | 2026-01-19 02:11:19.069Z | 234.929° WSW | 2026-01-19 02:13:19.069Z | 198.724° SSW | 19.041° | 2026-01-19 02:15:19.069Z | 164.639° 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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