YAOGAN-30 G, 43081
Orbit data source: Space-Track
YAOGAN-30 G, 43081 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Mon, 25 Dec 2017 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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43081 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: 1 day ago
TLE from 1 day ago
0 YAOGAN-30 G
1 43081U 17085A 26172.33850470 .00001797 00000-0 13406-3 0 9996
2 43081 34.9949 124.7508 0005044 197.1000 162.9538 15.02705577463347Epoch: 2026-06-21T08:07Z
TLE epoch observation values (Epoch: 2026-06-21T08:07:26.806Z)
Latitude
-0.00005°
Longitude
93.34884°
Altitude
560.818 km
Speed
7.581 km/s
True Right ascension
08h 19m 00s
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
21:31:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.28 km
Perigee altitude
558.279 km
Semi-major axis
6,939.917 km
Eccentricity
0.0005
Inclination
34.9949°
RAAN
124.7508°
Arg. of periapsis
197.1°
True anomaly
162.97073°
Mean anomaly
162.9538°
Eccentric anomaly
162.96227°
Mean motion
3.75415 °/min
Orbital period
95.89 mins
BSTAR
0.00013406
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Other satellites on launch #85 in the year 2017 (2017-12-25 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 G 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 | 2026-06-23 00:13:09.744Z | 210.015° SW | 2026-06-23 00:16:09.744Z | 162.349° S | 21.024° | 2026-06-23 00:19:09.744Z | 111.794° ESE |
| 6 mins | 2026-06-23 01:54:09.744Z | 238.119° WSW | 2026-06-23 01:57:09.744Z | 170.655° S | 32.928° | 2026-06-23 02:00:09.744Z | 109.792° ESE |
| 6 mins | 2026-06-23 03:35:09.744Z | 249.301° W | 2026-06-23 03:38:09.744Z | 183.277° SSW | 30.196° | 2026-06-23 03:41:09.744Z | 127.835° SE |
| 4 mins | 2026-06-23 05:17:09.744Z | 229.107° WSW | 2026-06-23 05:18:09.744Z | 212.928° SW | 15.656° | 2026-06-23 05:21:09.744Z | 166.535° S |
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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