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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 U
1 46807U 20076A 26306.48293001 .00001620 00000-0 11950-3 0 9992
2 46807 34.9948 327.9510 0000687 262.3323 97.7307 15.03210221328938Epoch: 2026-11-02T11:35Z
TLE epoch observation values (Epoch: 2026-11-02T11:35:25.152Z)
Latitude
-0.00005°
Longitude
112.33682°
Altitude
555.985 km
Speed
7.586 km/s
True Right ascension
21h 51m 48s
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
15:56:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.705 km
Perigee altitude
559.751 km
Semi-major axis
6,938.365 km
Eccentricity
0.00007
Inclination
34.9948°
RAAN
327.951°
Arg. of periapsis
262.3323°
True anomaly
97.7385°
Mean anomaly
97.7307°
Eccentric anomaly
97.7346°
Mean motion
3.75541 °/min
Orbital period
95.86 mins
BSTAR
0.0001195
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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 | 2026-11-03 05:21:28.284Z | 207.411° SW | 2026-11-03 05:24:28.284Z | 157.034° SSE | 22.397° | 2026-11-03 05:27:28.284Z | 109.447° ESE |
| 6 mins | 2026-11-03 07:02:28.284Z | 235.772° WSW | 2026-11-03 07:05:28.284Z | 159.883° S | 39.75° | 2026-11-03 07:08:28.284Z | 107.49° ESE |
| 6 mins | 2026-11-03 08:43:28.284Z | 246.79° WSW | 2026-11-03 08:45:28.284Z | 206.951° SW | 35.322° | 2026-11-03 08:49:28.284Z | 124.879° SE |
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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