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, Unknown HBR
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-30 U
1 46807U 20076A 25259.61748549 .00002957 00000-0 23133-3 0 9995
2 46807 34.9948 316.3345 0001003 237.8955 122.1656 15.00648695266968Epoch: 2025-09-16T14:49Z
TLE epoch observation values (Epoch: 2025-09-16T14:49:10.746Z)
Latitude
0.00003°
Longitude
98.23456°
Altitude
564.183 km
Speed
7.581 km/s
True Right ascension
21h 05m 20s
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
15:56:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.811 km
Perigee altitude
567.417 km
Semi-major axis
6,946.251 km
Eccentricity
0.0001
Inclination
34.9948°
RAAN
316.3345°
Arg. of periapsis
237.8955°
True anomaly
122.17533°
Mean anomaly
122.1656°
Eccentric anomaly
122.17046°
Mean motion
3.74902 °/min
Orbital period
96.03 mins
BSTAR
0.00023133
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 07:00:26.980Z | 180.595° SSW | 2025-09-17 07:02:26.980Z | 149.643° SSE | 14.425° | 2025-09-17 07:04:26.980Z | 120.8° SE |
| 6 mins | 2025-09-17 08:40:26.980Z | 223.003° SW | 2025-09-17 08:43:26.980Z | 153.111° SSE | 28.677° | 2025-09-17 08:46:26.980Z | 105.306° ESE |
| 6 mins | 2025-09-17 10:21:26.980Z | 244.824° WSW | 2025-09-17 10:24:26.980Z | 166.146° S | 32.784° | 2025-09-17 10:27:26.980Z | 116.018° SE |
| 4 mins | 2025-09-17 12:03:26.980Z | 230.559° WSW | 2025-09-17 12:05:26.980Z | 187.305° SSW | 22.281° | 2025-09-17 12:07:26.980Z | 153.015° 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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