YAOGAN-30 D, 43028
Orbit data source: Space-Track
YAOGAN-30 D, 43028 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Fri, 24 Nov 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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43028 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, 0.5 m
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-30 D
1 43028U 17075A 25312.08177605 .00005032 00000-0 38673-3 0 9994
2 43028 34.9926 176.9288 0001789 213.0118 147.0478 15.01158633433985Epoch: 2025-11-08T01:57Z
TLE epoch observation values (Epoch: 2025-11-08T01:57:45.450Z)
Latitude
-0.00003°
Longitude
99.97287°
Altitude
563.281 km
Speed
7.581 km/s
True Right ascension
11h 47m 42s
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
10:09:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.785 km
Perigee altitude
565.3 km
Semi-major axis
6,944.68 km
Eccentricity
0.00018
Inclination
34.9926°
RAAN
176.9288°
Arg. of periapsis
213.0118°
True anomaly
147.05895°
Mean anomaly
147.0478°
Eccentric anomaly
147.05337°
Mean motion
3.75029 °/min
Orbital period
95.99 mins
BSTAR
0.00038673
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Other satellites on launch #75 in the year 2017 (2017-11-24 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 D 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 | 2025-11-08 19:48:21.546Z | 219.751° SW | 2025-11-08 19:50:21.546Z | 180.41° SSW | 27.862° | 2025-11-08 19:54:21.546Z | 104.712° ESE |
| 6 mins | 2025-11-08 21:29:21.546Z | 242.815° WSW | 2025-11-08 21:31:21.546Z | 199.86° SSW | 33.022° | 2025-11-08 21:35:21.546Z | 113.861° SE |
| 5 mins | 2025-11-08 23:10:21.546Z | 243.407° WSW | 2025-11-08 23:12:21.546Z | 206.653° SW | 23.564° | 2025-11-08 23:15:21.546Z | 148.861° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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