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: 13 hours ago
TLE from 13 hours ago
0 YAOGAN-30 D
1 43028U 17075A 26278.27857938 .00001907 00000-0 14004-3 0 9990
2 43028 34.9954 319.1482 0002036 206.8770 153.1833 15.03267320483820Epoch: 2026-10-05T06:41Z
TLE epoch observation values (Epoch: 2026-10-05T06:41:09.258Z)
Latitude
-0.00002°
Longitude
-155.10017°
Altitude
557.005 km
Speed
7.585 km/s
True Right ascension
21h 16m 35s
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
13:24:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.465 km
Perigee altitude
558.64 km
Semi-major axis
6,938.189 km
Eccentricity
0.0002
Inclination
34.9954°
RAAN
319.1482°
Arg. of periapsis
206.877°
True anomaly
153.19382°
Mean anomaly
153.1833°
Eccentric anomaly
153.18856°
Mean motion
3.75555 °/min
Orbital period
95.86 mins
BSTAR
0.00014004
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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 | 2026-10-06 06:50:51.786Z | 212.867° SW | 2026-10-06 06:53:51.786Z | 156.1° SSE | 26.362° | 2026-10-06 06:56:51.786Z | 107.282° ESE |
| 6 mins | 2026-10-06 08:31:51.786Z | 239.38° WSW | 2026-10-06 08:34:51.786Z | 158.836° S | 40.767° | 2026-10-06 08:37:51.786Z | 109.064° ESE |
| 6 mins | 2026-10-06 10:12:51.786Z | 245.386° WSW | 2026-10-06 10:14:51.786Z | 204.905° SW | 32.266° | 2026-10-06 10:18:51.786Z | 129.926° SE |
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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