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, 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 V
1 46808U 20076B 25311.28341044 .00004396 00000-0 33861-3 0 9995
2 46808 34.9960 2.0914 0002506 226.7049 133.3450 15.01112572274847Epoch: 2025-11-07T06:48Z
TLE epoch observation values (Epoch: 2025-11-07T06:48:06.662Z)
Latitude
0°
Longitude
-146.66595°
Altitude
563.575 km
Speed
7.581 km/s
True Right ascension
00h 08m 21s
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
13:28:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.424 km
Perigee altitude
564.944 km
Semi-major axis
6,944.821 km
Eccentricity
0.00025
Inclination
34.996°
RAAN
2.0914°
Arg. of periapsis
226.7049°
True anomaly
133.36588°
Mean anomaly
133.345°
Eccentric anomaly
133.35544°
Mean motion
3.75018 °/min
Orbital period
96 mins
BSTAR
0.00033861
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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 | 2025-11-08 06:58:01.575Z | 204.408° SW | 2025-11-08 07:01:01.575Z | 158.35° S | 18.903° | 2025-11-08 07:04:01.575Z | 111.728° ESE |
| 6 mins | 2025-11-08 08:39:01.575Z | 234.463° WSW | 2025-11-08 08:42:01.575Z | 167.939° S | 32.077° | 2025-11-08 08:45:01.575Z | 108.694° ESE |
| 6 mins | 2025-11-08 10:20:01.575Z | 249.726° W | 2025-11-08 10:23:01.575Z | 184.144° SSW | 31.77° | 2025-11-08 10:26:01.575Z | 124.749° SE |
| 4 mins | 2025-11-08 12:02:01.575Z | 233.144° WSW | 2025-11-08 12:04:01.575Z | 197.496° SSW | 18.17° | 2025-11-08 12:06:01.575Z | 165.082° 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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