YAOGAN-30 U, 46807
Orbit data source: Space-Track
YAOGAN-30 U, 46807 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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46807 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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-30 U
1 46807U 20076A 26126.52025125 .00002705 00000-0 20173-3 0 9999
2 46807 34.9952 345.1563 0001040 286.8121 73.2473 15.02507383301845Epoch: 2026-05-06T12:29Z
TLE epoch observation values (Epoch: 2026-05-06T12:29:09.708Z)
Latitude
-0.00004°
Longitude
-66.51376°
Altitude
557.876 km
Speed
7.585 km/s
True Right ascension
23h 00m 37s
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
02:28:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.111 km
Perigee altitude
561.668 km
Semi-major axis
6,940.526 km
Eccentricity
0.0001
Inclination
34.9952°
RAAN
345.1563°
Arg. of periapsis
286.8121°
True anomaly
73.25871°
Mean anomaly
73.2473°
Eccentric anomaly
73.25301°
Mean motion
3.75366 °/min
Orbital period
95.91 mins
BSTAR
0.00020173
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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 U 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 | 2026-05-06 19:07:39.413Z | 218.034° SW | 2026-05-06 19:10:39.413Z | 160.203° S | 25.732° | 2026-05-06 19:13:39.413Z | 107.945° ESE |
| 6 mins | 2026-05-06 20:48:39.413Z | 242.887° WSW | 2026-05-06 20:51:39.413Z | 167.817° S | 33.554° | 2026-05-06 20:54:39.413Z | 112.306° ESE |
| 6 mins | 2026-05-06 22:29:39.413Z | 246.85° WSW | 2026-05-06 22:32:39.413Z | 183.564° SSW | 26.013° | 2026-05-06 22:35:39.413Z | 135.751° 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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