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: 3 hours ago
TLE from 3 hours ago
0 YAOGAN-30 D
1 43028U 17075A 26009.32028612 .00003811 00000-0 28904-3 0 9997
2 43028 34.9933 158.3054 0002097 344.1911 15.8731 15.01737066443346Epoch: 2026-01-09T07:41Z
TLE epoch observation values (Epoch: 2026-01-09T07:41:12.720Z)
Latitude
-0.00004°
Longitude
-65.85938°
Altitude
559.057 km
Speed
7.585 km/s
True Right ascension
10h 33m 13s
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
11:20:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.217 km
Perigee altitude
563.305 km
Semi-major axis
6,942.898 km
Eccentricity
0.00021
Inclination
34.9933°
RAAN
158.3054°
Arg. of periapsis
344.1911°
True anomaly
15.87967°
Mean anomaly
15.8731°
Eccentric anomaly
15.87639°
Mean motion
3.75173 °/min
Orbital period
95.96 mins
BSTAR
0.00028904
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-09 14:20:49.124Z | 204.347° SW | 2026-01-09 14:22:49.124Z | 158.933° S | 25.394° | 2026-01-09 14:25:49.124Z | 107.726° ESE |
| 6 mins | 2026-01-09 16:00:49.124Z | 242.573° WSW | 2026-01-09 16:03:49.124Z | 167.955° S | 33.615° | 2026-01-09 16:06:49.124Z | 112.037° ESE |
| 6 mins | 2026-01-09 17:41:49.124Z | 247.653° W | 2026-01-09 17:44:49.124Z | 184.995° SSW | 26.537° | 2026-01-09 17:47:49.124Z | 135.559° 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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