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: 3 hours ago
TLE from 3 hours ago
0 YAOGAN-30 D
1 43028U 17075A 26098.64974712 .00002797 00000-0 20874-3 0 9991
2 43028 34.9956 334.3331 0001226 23.5841 336.4923 15.02470278456785Epoch: 2026-04-08T15:35Z
TLE epoch observation values (Epoch: 2026-04-08T15:35:38.151Z)
Latitude
-0.00002°
Longitude
-96.48496°
Altitude
557.419 km
Speed
7.586 km/s
True Right ascension
22h 17m 19s
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
01:09:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.354 km
Perigee altitude
561.653 km
Semi-major axis
6,940.64 km
Eccentricity
0.00012
Inclination
34.9956°
RAAN
334.3331°
Arg. of periapsis
23.5841°
True anomaly
336.4867°
Mean anomaly
336.4923°
Eccentric anomaly
336.4895°
Mean motion
3.75356 °/min
Orbital period
95.91 mins
BSTAR
0.00020874
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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 | 2026-04-08 20:40:02.069Z | 221.082° SW | 2026-04-08 20:42:02.069Z | 181.075° SSW | 28.259° | 2026-04-08 20:46:02.069Z | 104.621° ESE |
| 6 mins | 2026-04-08 22:21:02.069Z | 242.271° WSW | 2026-04-08 22:23:02.069Z | 196.515° SSW | 33.08° | 2026-04-08 22:27:02.069Z | 114.125° SE |
| 5 mins | 2026-04-09 00:02:02.069Z | 240.61° WSW | 2026-04-09 00:04:02.069Z | 202.115° SSW | 22.993° | 2026-04-09 00:07:02.069Z | 148.125° SSE |
| 4 mins | 2026-04-09 18:57:02.069Z | 179.394° S | 2026-04-09 18:58:02.069Z | 161.583° S | 17.499° | 2026-04-09 19:01:02.069Z | 114.319° SE |
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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