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: 11 hours ago
TLE from 11 hours ago
0 YAOGAN-30 W
1 46809U 20076C 25314.98404531 .00006294 00000-0 48218-3 0 9998
2 46809 34.9972 339.4254 0006315 312.3472 47.6700 15.01214439275312Epoch: 2025-11-10T23:37Z
TLE epoch observation values (Epoch: 2025-11-10T23:37:01.514Z)
Latitude
-0.00006°
Longitude
-65.20811°
Altitude
559.118 km
Speed
7.586 km/s
True Right ascension
22h 37m 42s
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
06:40:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.755 km
Perigee altitude
561.984 km
Semi-major axis
6,944.507 km
Eccentricity
0.00063
Inclination
34.9972°
RAAN
339.4254°
Arg. of periapsis
312.3472°
True anomaly
47.72353°
Mean anomaly
47.67°
Eccentric anomaly
47.69676°
Mean motion
3.75043 °/min
Orbital period
95.99 mins
BSTAR
0.00048218
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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 | 2025-11-12 06:13:32.329Z | 223.202° SW | 2025-11-12 06:16:32.329Z | 158.381° S | 28.426° | 2025-11-12 06:19:32.329Z | 106.583° ESE |
| 6 mins | 2025-11-12 07:54:32.329Z | 245.533° WSW | 2025-11-12 07:57:32.329Z | 170.613° S | 33.419° | 2025-11-12 08:00:32.329Z | 115.758° SE |
| 5 mins | 2025-11-12 09:36:32.329Z | 232.798° WSW | 2025-11-12 09:38:32.329Z | 188.918° SSW | 23.381° | 2025-11-12 09:41:32.329Z | 142.64° 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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