TIANHUI 7, 67300
Orbit data source: Space-Track
TIANHUI 7, 67300 is a payload satellite owned by G. Cehui dili (CN) in SSO that was launched on Tue, 30 Dec 2025 UTC via a CHANG ZHENG 4B 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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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Civil 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, 14.5 m
Radar Cross Section
2.045 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TIANHUI 7
1 67300U 25314A 26170.19660604 .00004815 00000-0 19030-3 0 9993
2 67300 97.4024 245.8440 0001665 298.0319 62.0751 15.25965892 26091Epoch: 2026-06-19T04:43Z
TLE epoch observation values (Epoch: 2026-06-19T04:43:06.761Z)
Latitude
-0.00003°
Longitude
-92.36322°
Altitude
490.45 km
Speed
7.62 km/s
True Right ascension
16h 23m 22s
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
07:22:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.987 km
Perigee altitude
483.702 km
Semi-major axis
6,862.981 km
Eccentricity
0.00017
Inclination
97.4024°
RAAN
245.844°
Arg. of periapsis
298.0319°
True anomaly
62.09196°
Mean anomaly
62.0751°
Eccentric anomaly
62.08353°
Mean motion
3.81746 °/min
Orbital period
94.3 mins
BSTAR
0.0001903
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Other satellites on launch #314 in the year 2025 (2025-12-30 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 7 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 05:39:00.565Z | 216.39° SW | 2026-06-21 05:41:00.565Z | 277.221° WNW | 27.491° | 2026-06-21 05:43:00.565Z | 320.237° NNW |
| 4 mins | 2026-06-21 18:40:00.565Z | 329.721° NNW | 2026-06-21 18:42:00.565Z | 282.581° WNW | 21.949° | 2026-06-21 18:44:00.565Z | 241.958° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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