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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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, Unknown HBR
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 V
1 46808U 20076B 25259.59664876 .00002943 00000-0 23060-3 0 9997
2 46808 34.9953 316.2308 0001669 152.1398 207.9399 15.00589364267077Epoch: 2025-09-16T14:19Z
TLE epoch observation values (Epoch: 2025-09-16T14:19:10.452Z)
Latitude
-0.00004°
Longitude
105.65252°
Altitude
565.019 km
Speed
7.58 km/s
True Right ascension
21h 04m 55s
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
15:57:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.456 km
Perigee altitude
567.137 km
Semi-major axis
6,946.434 km
Eccentricity
0.00017
Inclination
34.9953°
RAAN
316.2308°
Arg. of periapsis
152.1398°
True anomaly
207.93094°
Mean anomaly
207.9399°
Eccentric anomaly
207.93542°
Mean motion
3.74887 °/min
Orbital period
96.03 mins
BSTAR
0.0002306
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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 | 2025-09-17 08:08:29.407Z | 217.663° SW | 2025-09-17 08:11:29.407Z | 162.851° S | 25.308° | 2025-09-17 08:14:29.407Z | 109.157° ESE |
| 6 mins | 2025-09-17 09:49:29.407Z | 244.072° WSW | 2025-09-17 09:52:29.407Z | 177.318° S | 33.981° | 2025-09-17 09:55:29.407Z | 113.301° SE |
| 5 mins | 2025-09-17 11:31:29.407Z | 239.31° WSW | 2025-09-17 11:33:29.407Z | 193.667° SSW | 27.15° | 2025-09-17 11:36:29.407Z | 137.553° 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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