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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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-32 A
1 43642U 18077A 25309.96078792 .00000934 00000-0 19160-3 0 9995
2 43642 97.9281 338.2566 0001482 98.9723 261.1647 14.62846241377207Epoch: 2025-11-05T23:03Z
TLE epoch observation values (Epoch: 2025-11-05T23:03:32.076Z)
Latitude
-0.00004°
Longitude
-53.053°
Altitude
687.157 km
Speed
7.513 km/s
True Right ascension
22h 33m 01s
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
04:29:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
682.11 km
Perigee altitude
680.018 km
Semi-major axis
7,059.201 km
Eccentricity
0.00015
Inclination
97.9281°
RAAN
338.2566°
Arg. of periapsis
98.9723°
True anomaly
261.14792°
Mean anomaly
261.1647°
Eccentric anomaly
261.15631°
Mean motion
3.6594 °/min
Orbital period
98.38 mins
BSTAR
0.0001916
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-06 14:24:53.565Z | 30.971° NE | 2025-11-06 14:28:53.565Z | 113.997° SE | 33.615° | 2025-11-06 14:31:53.565Z | 165.138° S |
| 4 mins | 2025-11-06 16:03:53.565Z | 320.648° NNW | 2025-11-06 16:05:53.565Z | 288.169° WNW | 17.866° | 2025-11-06 16:07:53.565Z | 258.881° W |
| 7 mins | 2025-11-07 01:27:53.565Z | 132.264° SE | 2025-11-07 01:30:53.565Z | 74.664° E | 32.348° | 2025-11-07 01:34:53.565Z | 5.152° NNE |
| 4 mins | 2025-11-07 03:06:53.565Z | 240.073° WSW | 2025-11-07 03:08:53.565Z | 273.286° WNW | 18.332° | 2025-11-07 03:10:53.565Z | 303.14° 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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