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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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: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-30 D
1 43028U 17075A 26172.53269884 .00001767 00000-0 13138-3 0 9990
2 43028 34.9940 244.0445 0002109 330.0106 30.0482 15.02842120467904Epoch: 2026-06-21T12:47Z
TLE epoch observation values (Epoch: 2026-06-21T12:47:05.179Z)
Latitude
0.00002°
Longitude
142.54133°
Altitude
555.788 km
Speed
7.587 km/s
True Right ascension
16h 16m 10s
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
21:39:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.823 km
Perigee altitude
559.896 km
Semi-major axis
6,939.497 km
Eccentricity
0.00021
Inclination
34.994°
RAAN
244.0445°
Arg. of periapsis
330.0106°
True anomaly
30.0603°
Mean anomaly
30.0482°
Eccentric anomaly
30.05425°
Mean motion
3.75449 °/min
Orbital period
95.89 mins
BSTAR
0.00013138
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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 | 2026-06-22 11:29:26.239Z | 249.524° W | 2026-06-22 11:32:26.239Z | 184.097° SSW | 32.511° | 2026-06-22 11:35:26.239Z | 122.182° SE |
| 4 mins | 2026-06-22 13:11:26.239Z | 233.049° WSW | 2026-06-22 13:13:26.239Z | 194.698° SSW | 19.818° | 2026-06-22 13:15:26.239Z | 160.763° S |
| 4 mins | 2026-06-23 08:05:26.239Z | 188.759° SSW | 2026-06-23 08:06:26.239Z | 169.733° S | 20.256° | 2026-06-23 08:09:26.239Z | 115.7° SE |
| 6 mins | 2026-06-23 09:45:26.239Z | 231.332° WSW | 2026-06-23 09:47:26.239Z | 183.677° SSW | 32.565° | 2026-06-23 09:51:26.239Z | 105.671° ESE |
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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