TIANHUI 5D, 60212
Orbit data source: Space-Track
TIANHUI 5D, 60212 is a payload satellite owned by G. Cehui dili (CN) in SSO that was launched on Thu, 04 Jul 2024 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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60212 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational spacecraft
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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 TIANHUI 5D
1 60212U 24126B 25253.95154895 .00000402 00000-0 50249-4 0 9999
2 60212 97.8203 260.5362 0002116 92.9847 267.1612 14.87578549 64389Epoch: 2025-09-10T22:50Z
TLE epoch observation values (Epoch: 2025-09-10T22:50:13.829Z)
Latitude
0.00004°
Longitude
-72.24202°
Altitude
608.612 km
Speed
7.555 km/s
True Right ascension
17h 22m 08s
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
07:35:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.008 km
Perigee altitude
601.054 km
Semi-major axis
6,980.668 km
Eccentricity
0.00021
Inclination
97.8203°
RAAN
260.5362°
Arg. of periapsis
92.9847°
True anomaly
267.13698°
Mean anomaly
267.1612°
Eccentric anomaly
267.14909°
Mean motion
3.72133 °/min
Orbital period
96.74 mins
BSTAR
0.000050249
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Other satellites on launch #126 in the year 2024 (2024-07-04 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 5D 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-13 23:38:16.979Z | 109.433° ESE | 2025-09-13 23:40:16.979Z | 75.822° E | 20.267° | 2025-09-13 23:43:16.979Z | 23.565° NE |
| 5 mins | 2025-09-14 01:14:16.979Z | 218.711° SW | 2025-09-14 01:16:16.979Z | 262.851° W | 26.386° | 2025-09-14 01:19:16.979Z | 319.285° NNW |
| 6 mins | 2025-09-14 12:59:16.979Z | 37.851° NE | 2025-09-14 13:01:16.979Z | 83.544° E | 33.956° | 2025-09-14 13:05:16.979Z | 169.582° S |
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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