YAOGAN-30 J, 43083
Orbit data source: Space-Track
YAOGAN-30 J, 43083 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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43083 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 J
1 43083U 17085C 26172.31787596 .00001813 00000-0 13508-3 0 9996
2 43083 34.9942 125.3898 0005057 183.6844 176.3827 15.02740635463378Epoch: 2026-06-21T07:37Z
TLE epoch observation values (Epoch: 2026-06-21T07:37:44.482Z)
Latitude
-0.00007°
Longitude
101.43449°
Altitude
560.866 km
Speed
7.581 km/s
True Right ascension
08h 21m 33s
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
21:26:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.181 km
Perigee altitude
558.163 km
Semi-major axis
6,939.809 km
Eccentricity
0.00051
Inclination
34.9942°
RAAN
125.3898°
Arg. of periapsis
183.6844°
True anomaly
176.38635°
Mean anomaly
176.3827°
Eccentric anomaly
176.38453°
Mean motion
3.75424 °/min
Orbital period
95.89 mins
BSTAR
0.00013508
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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 J 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 | 2026-06-22 23:42:21.400Z | 193.227° SSW | 2026-06-22 23:45:21.400Z | 147.18° SSE | 15.578° | 2026-06-22 23:47:21.400Z | 118.098° SE |
| 6 mins | 2026-06-23 01:23:21.400Z | 222.315° SW | 2026-06-23 01:25:21.400Z | 176.759° S | 30.095° | 2026-06-23 01:29:21.400Z | 103.62° ESE |
| 6 mins | 2026-06-23 03:04:21.400Z | 240.705° WSW | 2026-06-23 03:06:21.400Z | 189.33° SSW | 32.941° | 2026-06-23 03:10:21.400Z | 115.539° SE |
| 5 mins | 2026-06-23 04:45:21.400Z | 236.19° WSW | 2026-06-23 04:47:21.400Z | 197.485° SSW | 21.076° | 2026-06-23 04:50:21.400Z | 149.604° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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