YAOGAN-30 E, 43029
Orbit data source: Space-Track
YAOGAN-30 E, 43029 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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43029 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 E
1 43029U 17075B 26172.52352804 .00001734 00000-0 12942-3 0 9991
2 43029 34.9938 243.8053 0004072 278.5918 81.4329 15.02713062468017Epoch: 2026-06-21T12:33Z
TLE epoch observation values (Epoch: 2026-06-21T12:33:52.822Z)
Latitude
-0.00001°
Longitude
145.61262°
Altitude
557.031 km
Speed
7.586 km/s
True Right ascension
16h 15m 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
21:40:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.583 km
Perigee altitude
558.931 km
Semi-major axis
6,939.894 km
Eccentricity
0.00041
Inclination
34.9938°
RAAN
243.8053°
Arg. of periapsis
278.5918°
True anomaly
81.47904°
Mean anomaly
81.4329°
Eccentric anomaly
81.45597°
Mean motion
3.75417 °/min
Orbital period
95.89 mins
BSTAR
0.00012942
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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 E 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 11:15:14.205Z | 251.672° W | 2026-06-22 11:18:14.205Z | 200.728° SSW | 32.594° | 2026-06-22 11:22:14.205Z | 116.08° SE |
| 5 mins | 2026-06-22 12:57:14.205Z | 240.946° WSW | 2026-06-22 12:59:14.205Z | 204.261° SW | 21.901° | 2026-06-22 13:02:14.205Z | 151.169° SSE |
| 4 mins | 2026-06-23 07:52:14.205Z | 178.619° S | 2026-06-23 07:53:14.205Z | 159.631° S | 18.731° | 2026-06-23 07:56:14.205Z | 112.334° ESE |
| 6 mins | 2026-06-23 09:31:14.205Z | 234.048° WSW | 2026-06-23 09:34:14.205Z | 166.127° S | 31.896° | 2026-06-23 09:37:14.205Z | 108.334° ESE |
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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