YAOGAN-32 2B, 49384
Orbit data source: Space-Track
YAOGAN-32 2B, 49384 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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49384 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: 23 hours ago
TLE from 23 hours ago
0 YAOGAN-32 2B
1 49384U 21099B 26172.54371644 .00000504 00000-0 10491-3 0 9998
2 49384 98.2472 306.3671 0001048 117.4548 242.6761 14.64213236247004Epoch: 2026-06-21T13:02Z
TLE epoch observation values (Epoch: 2026-06-21T13:02:57.100Z)
Latitude
-0.00001°
Longitude
-159.11329°
Altitude
682.932 km
Speed
7.515 km/s
True Right ascension
20h 25m 28s
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
23:08:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
677.42 km
Perigee altitude
675.941 km
Semi-major axis
7,054.817 km
Eccentricity
0.0001
Inclination
98.2472°
RAAN
306.3671°
Arg. of periapsis
117.4548°
True anomaly
242.66543°
Mean anomaly
242.6761°
Eccentric anomaly
242.67077°
Mean motion
3.66281 °/min
Orbital period
98.29 mins
BSTAR
0.00010491
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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 2B 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 20:48:32.146Z | 53.229° ENE | 2026-06-22 20:51:32.146Z | 98.421° ESE | 18.29° | 2026-06-22 20:54:32.146Z | 139.51° SSE |
| 7 mins | 2026-06-22 22:25:32.146Z | 350.49° N | 2026-06-22 22:28:32.146Z | 293.464° NW | 32.353° | 2026-06-22 22:32:32.146Z | 222.91° SW |
| 5 mins | 2026-06-23 07:51:32.146Z | 98.222° ESE | 2026-06-23 07:53:32.146Z | 66.911° ENE | 18.457° | 2026-06-23 07:56:32.146Z | 23.406° NE |
| 7 mins | 2026-06-23 09:27:32.146Z | 198.372° SSW | 2026-06-23 09:30:32.146Z | 259.794° W | 33.428° | 2026-06-23 09:34:32.146Z | 330.2° 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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