YAOGAN-32 2A, 49383
Orbit data source: Space-Track
YAOGAN-32 2A, 49383 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Wed, 03 Nov 2021 UTC via a CHANG ZHENG 2C/YZ-1S 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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49383 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: 21 hours ago
TLE from 21 hours ago
0 YAOGAN-32 2A
1 49383U 21099A 26172.54385023 .00000511 00000-0 10635-3 0 9991
2 49383 98.2477 306.3578 0001505 143.6213 216.5092 14.64215865247009Epoch: 2026-06-21T13:03Z
TLE epoch observation values (Epoch: 2026-06-21T13:03:08.659Z)
Latitude
-0.00002°
Longitude
-159.17088°
Altitude
683.437 km
Speed
7.514 km/s
True Right ascension
20h 25m 25s
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
21:31:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
677.734 km
Perigee altitude
675.61 km
Semi-major axis
7,054.809 km
Eccentricity
0.00015
Inclination
98.2477°
RAAN
306.3578°
Arg. of periapsis
143.6213°
True anomaly
216.49894°
Mean anomaly
216.5092°
Eccentric anomaly
216.50407°
Mean motion
3.66282 °/min
Orbital period
98.28 mins
BSTAR
0.00010635
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Other satellites on launch #99 in the year 2021 (2021-11-03 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-32 2A 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 | 2026-06-22 20:48:16.917Z | 48.693° ENE | 2026-06-22 20:51:16.917Z | 90.645° ESE | 18.41° | 2026-06-22 20:54:16.917Z | 135.311° SSE |
| 6 mins | 2026-06-22 22:26:16.917Z | 345.415° N | 2026-06-22 22:29:16.917Z | 275.06° WNW | 31.732° | 2026-06-22 22:32:16.917Z | 225.741° WSW |
| 4 mins | 2026-06-23 07:52:16.917Z | 90.718° ESE | 2026-06-23 07:54:16.917Z | 57.071° ENE | 18.292° | 2026-06-23 07:56:16.917Z | 27.966° NE |
| 6 mins | 2026-06-23 09:28:16.917Z | 203.827° SW | 2026-06-23 09:30:16.917Z | 244.645° WSW | 32.607° | 2026-06-23 09:34:16.917Z | 327.469° NNW |
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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