YAOGAN-32 A, 43642
Orbit data source: Space-Track
YAOGAN-32 A, 43642 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Tue, 09 Oct 2018 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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43642 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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-32 A
1 43642U 18077A 26265.29549669 .00000232 00000-0 54167-4 0 9997
2 43642 98.1437 292.6540 0001124 98.7564 261.3765 14.63270316424045Epoch: 2026-09-22T07:05Z
TLE epoch observation values (Epoch: 2026-09-22T07:05:30.914Z)
Latitude
-0.00003°
Longitude
-174.88782°
Altitude
685.745 km
Speed
7.514 km/s
True Right ascension
19h 30m 36s
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
06:47:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
680.502 km
Perigee altitude
678.915 km
Semi-major axis
7,057.845 km
Eccentricity
0.00011
Inclination
98.1437°
RAAN
292.654°
Arg. of periapsis
98.7564°
True anomaly
261.36377°
Mean anomaly
261.3765°
Eccentric anomaly
261.37013°
Mean motion
3.66045 °/min
Orbital period
98.35 mins
BSTAR
0.000054167
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Other satellites on launch #77 in the year 2018 (2018-10-09 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 A 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 | 2026-09-22 14:13:40.363Z | 30.303° NE | 2026-09-22 14:17:40.363Z | 90.624° ESE | 36.924° | 2026-09-22 14:21:40.363Z | 162.711° S |
| 5 mins | 2026-09-22 15:52:40.363Z | 331.099° NNW | 2026-09-22 15:54:40.363Z | 299.784° NW | 21.522° | 2026-09-22 15:57:40.363Z | 252.209° W |
| 6 mins | 2026-09-23 01:17:40.363Z | 122.962° SE | 2026-09-23 01:20:40.363Z | 57.892° ENE | 34.609° | 2026-09-23 01:23:40.363Z | 9.962° NNE |
| 5 mins | 2026-09-23 02:55:40.363Z | 232.084° WSW | 2026-09-23 02:57:40.363Z | 266.102° W | 21.99° | 2026-09-23 03:00:40.363Z | 311.416° NW |
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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