YAOGAN-33, 47302
Orbit data source: Space-Track
YAOGAN-33, 47302 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Sun, 27 Dec 2020 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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47302 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Radar 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, Unknown HBR
Radar Cross Section
4.795 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 YAOGAN-33
1 47302U 20103A 26172.54920660 .00000244 00000-0 61520-4 0 9990
2 47302 98.0414 53.9950 0004363 111.4669 248.6997 14.58883185291940Epoch: 2026-06-21T13:10Z
TLE epoch observation values (Epoch: 2026-06-21T13:10:51.450Z)
Latitude
0.00004°
Longitude
-53.46726°
Altitude
700.894 km
Speed
7.505 km/s
True Right ascension
03h 35m 58s
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
23:08:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
696.943 km
Perigee altitude
690.772 km
Semi-major axis
7,071.995 km
Eccentricity
0.00044
Inclination
98.0414°
RAAN
53.995°
Arg. of periapsis
111.4669°
True anomaly
248.65313°
Mean anomaly
248.6997°
Eccentric anomaly
248.67641°
Mean motion
3.64947 °/min
Orbital period
98.64 mins
BSTAR
0.00006152
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Other satellites on launch #103 in the year 2020 (2020-12-27 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-33 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 15:38:25.373Z | 143.055° SSE | 2026-06-22 15:42:25.373Z | 76.481° E | 35.759° | 2026-06-22 15:46:25.373Z | 2.233° NNE |
| 4 mins | 2026-06-22 17:18:25.373Z | 238.737° WSW | 2026-06-22 17:20:25.373Z | 268.129° W | 16.391° | 2026-06-22 17:22:25.373Z | 297.275° NW |
| 7 mins | 2026-06-23 05:16:25.373Z | 0.555° NNE | 2026-06-23 05:19:25.373Z | 273.163° WNW | 41.655° | 2026-06-23 05:23:25.373Z | 206.409° 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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