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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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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 U
1 46807U 20076A 26017.91922404 .00002830 00000-0 21534-3 0 9998
2 46807 34.9946 286.5425 0001006 276.7315 83.3279 15.01723146285504Epoch: 2026-01-17T22:03Z
TLE epoch observation values (Epoch: 2026-01-17T22:03:40.957Z)
Latitude
0.00003°
Longitude
-161.71536°
Altitude
560.418 km
Speed
7.583 km/s
True Right ascension
19h 06m 10s
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
08:12:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.502 km
Perigee altitude
564.105 km
Semi-major axis
6,942.94 km
Eccentricity
0.0001
Inclination
34.9946°
RAAN
286.5425°
Arg. of periapsis
276.7315°
True anomaly
83.33935°
Mean anomaly
83.3279°
Eccentric anomaly
83.33362°
Mean motion
3.7517 °/min
Orbital period
95.96 mins
BSTAR
0.00021534
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-18 22:17:04.403Z | 213.307° SW | 2026-01-18 22:19:04.403Z | 167.07° S | 27.932° | 2026-01-18 22:22:04.403Z | 109.069° ESE |
| 6 mins | 2026-01-18 23:57:04.403Z | 247° WSW | 2026-01-19 00:00:04.403Z | 180.432° SSW | 33.816° | 2026-01-19 00:03:04.403Z | 116.489° SE |
| 5 mins | 2026-01-19 01:39:04.403Z | 236.775° WSW | 2026-01-19 01:41:04.403Z | 193.715° SSW | 24.253° | 2026-01-19 01:44:04.403Z | 142.857° 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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