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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 V
1 46808U 20076B 26306.46201642 .00001637 00000-0 12072-3 0 9995
2 46808 34.9953 327.8612 0000644 162.0926 197.9805 15.03204874329041Epoch: 2026-11-02T11:05Z
TLE epoch observation values (Epoch: 2026-11-02T11:05:18.218Z)
Latitude
-0.00003°
Longitude
119.79655°
Altitude
556.362 km
Speed
7.585 km/s
True Right ascension
21h 51m 26s
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
15:56:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.691 km
Perigee altitude
559.797 km
Semi-major axis
6,938.381 km
Eccentricity
0.00006
Inclination
34.9953°
RAAN
327.8612°
Arg. of periapsis
162.0926°
True anomaly
197.97822°
Mean anomaly
197.9805°
Eccentric anomaly
197.97936°
Mean motion
3.7554 °/min
Orbital period
95.86 mins
BSTAR
0.00012072
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 04:50:28.098Z | 190.727° SSW | 2026-11-03 04:52:28.098Z | 160.386° S | 16.566° | 2026-11-03 04:55:28.098Z | 115.11° SE |
| 5 mins | 2026-11-03 06:31:28.098Z | 219.12° SW | 2026-11-03 06:33:28.098Z | 167.31° S | 36.188° | 2026-11-03 06:36:28.098Z | 108.031° ESE |
| 6 mins | 2026-11-03 08:11:28.098Z | 248.26° W | 2026-11-03 08:14:28.098Z | 177.095° S | 40.72° | 2026-11-03 08:17:28.098Z | 119.153° SE |
| 4 mins | 2026-11-03 09:53:28.098Z | 231.237° WSW | 2026-11-03 09:55:28.098Z | 190.138° SSW | 22.509° | 2026-11-03 09:57:28.098Z | 156.361° 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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