YAOGAN-30 V, 46808
Orbit data source: Space-Track
YAOGAN-30 V, 46808 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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46808 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 V
1 46808U 20076B 26172.41020183 .00002051 00000-0 15261-3 0 9994
2 46808 34.9951 65.2453 0000766 322.6831 37.3824 15.02728439308861Epoch: 2026-06-21T09:50Z
TLE epoch observation values (Epoch: 2026-06-21T09:50:41.438Z)
Latitude
0°
Longitude
7.96177°
Altitude
556.981 km
Speed
7.586 km/s
True Right ascension
04h 20m 58s
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
21:37:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.241 km
Perigee altitude
561.178 km
Semi-major axis
6,939.846 km
Eccentricity
0.00008
Inclination
34.9951°
RAAN
65.2453°
Arg. of periapsis
322.6831°
True anomaly
37.38773°
Mean anomaly
37.3824°
Eccentric anomaly
37.38506°
Mean motion
3.75421 °/min
Orbital period
95.89 mins
BSTAR
0.00015261
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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 V 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 21:12:35.215Z | 219.267° SW | 2026-06-22 21:14:35.215Z | 179.057° S | 27.799° | 2026-06-22 21:18:35.215Z | 104.365° ESE |
| 6 mins | 2026-06-22 22:53:35.215Z | 241.162° WSW | 2026-06-22 22:55:35.215Z | 193.678° SSW | 33.346° | 2026-06-22 22:59:35.215Z | 112.989° SE |
| 5 mins | 2026-06-23 00:34:35.215Z | 239.976° WSW | 2026-06-23 00:36:35.215Z | 199.998° SSW | 23.694° | 2026-06-23 00:39:35.215Z | 145.995° 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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