YAOGAN 19, 39410
Orbit data source: Space-Track
YAOGAN 19, 39410 is a payload satellite owned by PLA GAD (CN) in SSO that was launched on Wed, 20 Nov 2013 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). 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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39410 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Civil Imaging
Bus & Motor
JB-9, Unknown motor
Mass
1,040 kg wet, 1,040 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
4.795 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YAOGAN 19
1 39410U 13065A 26172.49861328 -.00000156 00000-0 -30048-3 0 9993
2 39410 100.1121 148.7056 0010185 78.0328 282.1926 13.15583210604211Epoch: 2026-06-21T11:58Z
TLE epoch observation values (Epoch: 2026-06-21T11:58:00.187Z)
Latitude
-0.00009°
Longitude
59.50682°
Altitude
1,202.738 km
Speed
7.253 km/s
True Right ascension
09h 54m 49s
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
00:38:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,206.724 km
Perigee altitude
1,191.289 km
Semi-major axis
7,577.143 km
Eccentricity
0.00102
Inclination
100.1121°
RAAN
148.7056°
Arg. of periapsis
78.0328°
True anomaly
282.07849°
Mean anomaly
282.1926°
Eccentric anomaly
282.13555°
Mean motion
3.29067 °/min
Orbital period
109.4 mins
BSTAR
-0.00030048
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Other satellites on launch #65 in the year 2013 (2013-11-20 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 19 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-22 20:58:17.295Z | 110.796° ESE | 2026-06-22 21:03:17.295Z | 60.648° ENE | 24.722° | 2026-06-22 21:08:17.295Z | 10.358° NNE |
| 12 mins | 2026-06-22 22:45:17.295Z | 183.628° SSW | 2026-06-22 22:50:17.295Z | 246.486° WSW | 40.31° | 2026-06-22 22:57:17.295Z | 336.283° NNW |
| 10 mins | 2026-06-23 10:14:17.295Z | 45.809° ENE | 2026-06-23 10:19:17.295Z | 101.632° ESE | 25.664° | 2026-06-23 10:24:17.295Z | 150.143° SSE |
| 12 mins | 2026-06-23 12:01:17.295Z | 2.229° NNE | 2026-06-23 12:07:17.295Z | 280.044° WNW | 38.114° | 2026-06-23 12:13:17.295Z | 219.647° SW |
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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