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: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-30 D
1 43028U 17075A 25261.99275752 .00003178 00000-0 24870-3 0 9992
2 43028 34.9937 121.3726 0000980 81.0506 279.0313 15.00606362426458Epoch: 2025-09-18T23:49Z
TLE epoch observation values (Epoch: 2025-09-18T23:49:34.249Z)
Latitude
0.00001°
Longitude
125.83351°
Altitude
563.836 km
Speed
7.582 km/s
True Right ascension
08h 05m 29s
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
00:36:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.925 km
Perigee altitude
567.564 km
Semi-major axis
6,946.382 km
Eccentricity
0.0001
Inclination
34.9937°
RAAN
121.3726°
Arg. of periapsis
81.0506°
True anomaly
279.02021°
Mean anomaly
279.0313°
Eccentric anomaly
279.02575°
Mean motion
3.74891 °/min
Orbital period
96.03 mins
BSTAR
0.0002487
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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 | 2025-09-19 19:16:11.171Z | 216.786° SW | 2025-09-19 19:18:11.171Z | 176.261° S | 27.392° | 2025-09-19 19:22:11.171Z | 104.034° ESE |
| 6 mins | 2025-09-19 20:57:11.171Z | 241.422° WSW | 2025-09-19 20:59:11.171Z | 196.385° SSW | 33.376° | 2025-09-19 21:03:11.171Z | 112.485° ESE |
| 5 mins | 2025-09-19 22:38:11.171Z | 243.413° WSW | 2025-09-19 22:40:11.171Z | 205.652° SW | 24.42° | 2025-09-19 22:43:11.171Z | 146.795° SSE |
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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