TIANHUI 5A, 58199
Orbit data source: Space-Track
TIANHUI 5A, 58199 is a payload satellite owned by G. Cehui dili (CN) in SSO that was launched on Tue, 31 Oct 2023 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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58199 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Civil Radar Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.0 m
Radar Cross Section
12.451 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TIANHUI 5A
1 58199U 23168A 25307.60575441 .00000598 00000-0 71816-4 0 9990
2 58199 97.8205 313.2284 0001555 88.3842 271.7552 14.87588245109064Epoch: 2025-11-03T14:32Z
TLE epoch observation values (Epoch: 2025-11-03T14:32:17.181Z)
Latitude
-0.00003°
Longitude
52.05209°
Altitude
608.475 km
Speed
7.555 km/s
True Right ascension
20h 52m 54s
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
18:20:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.586 km
Perigee altitude
601.415 km
Semi-major axis
6,980.638 km
Eccentricity
0.00016
Inclination
97.8205°
RAAN
313.2284°
Arg. of periapsis
88.3842°
True anomaly
271.73739°
Mean anomaly
271.7552°
Eccentric anomaly
271.74629°
Mean motion
3.72135 °/min
Orbital period
96.74 mins
BSTAR
0.000071816
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Other satellites on launch #168 in the year 2023 (2023-10-31 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.TIANHUI 5A 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 | 2025-11-05 00:33:27.363Z | 168.696° S | 2025-11-05 00:37:27.363Z | 324.66° NNW | 44.14° | 2025-11-05 00:40:27.363Z | 345.716° N |
| 6 mins | 2025-11-05 13:55:27.363Z | 349.769° N | 2025-11-05 13:58:27.363Z | 283.634° WNW | 32.057° | 2025-11-05 14:01:27.363Z | 224.477° SW |
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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