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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-32 A
1 43642U 18077A 25258.31583416 .00000871 00000-0 17973-3 0 9991
2 43642 97.9355 288.6217 0001339 87.6827 272.4529 14.62712832369653Epoch: 2025-09-15T07:34Z
TLE epoch observation values (Epoch: 2025-09-15T07:34:48.071Z)
Latitude
0.00002°
Longitude
-179.60084°
Altitude
687.385 km
Speed
7.513 km/s
True Right ascension
19h 14m 29s
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
05:50:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
682.439 km
Perigee altitude
680.548 km
Semi-major axis
7,059.631 km
Eccentricity
0.00013
Inclination
97.9355°
RAAN
288.6217°
Arg. of periapsis
87.6827°
True anomaly
272.43757°
Mean anomaly
272.4529°
Eccentric anomaly
272.44524°
Mean motion
3.65907 °/min
Orbital period
98.39 mins
BSTAR
0.00017973
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-15 14:42:37.463Z | 20.121° NNE | 2025-09-15 14:47:37.463Z | 129.186° SE | 39.998° | 2025-09-15 14:51:37.463Z | 180.912° SSW |
| 7 mins | 2025-09-16 01:46:37.463Z | 144.409° SSE | 2025-09-16 01:49:37.463Z | 75.402° E | 39.242° | 2025-09-16 01:53:37.463Z | 358.457° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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