YAOGAN-30 W, 46809
Orbit data source: Space-Track
YAOGAN-30 W, 46809 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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46809 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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 W
1 46809U 20076C 25259.57473895 .00003117 00000-0 24368-3 0 9991
2 46809 34.9967 316.2206 0006636 201.5259 158.5170 15.00636946266980Epoch: 2025-09-16T13:47Z
TLE epoch observation values (Epoch: 2025-09-16T13:47:37.445Z)
Latitude
-0.00002°
Longitude
113.55147°
Altitude
568.135 km
Speed
7.577 km/s
True Right ascension
21h 04m 52s
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
15:55:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.759 km
Perigee altitude
563.54 km
Semi-major axis
6,946.287 km
Eccentricity
0.00066
Inclination
34.9967°
RAAN
316.2206°
Arg. of periapsis
201.5259°
True anomaly
158.54483°
Mean anomaly
158.517°
Eccentric anomaly
158.53092°
Mean motion
3.74899 °/min
Orbital period
96.03 mins
BSTAR
0.00024368
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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 W 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 | 2025-09-17 07:35:04.863Z | 208.907° SW | 2025-09-17 07:38:04.863Z | 163.109° S | 20.399° | 2025-09-17 07:41:04.863Z | 112.882° SE |
| 6 mins | 2025-09-17 09:17:04.863Z | 228.888° WSW | 2025-09-17 09:19:04.863Z | 178.017° S | 32.809° | 2025-09-17 09:23:04.863Z | 104.778° ESE |
| 6 mins | 2025-09-17 10:58:04.863Z | 242.324° WSW | 2025-09-17 11:00:04.863Z | 194.866° SSW | 30.949° | 2025-09-17 11:04:04.863Z | 122.507° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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