QIANFAN-89, 63175
Orbit data source: Space-Track
QIANFAN-89, 63175 is a Chinese payload satellite in LEO that was launched on Tue, 11 Mar 2025 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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63175 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.8 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-89
1 63175U 25046S 26171.40491558 .00000119 00000-0 16519-3 0 9998
2 63175 88.9714 300.3669 0014572 299.1710 60.7983 13.51017544 73011Epoch: 2026-06-20T09:43Z
TLE epoch observation values (Epoch: 2026-06-20T09:43:04.706Z)
Latitude
0.00003°
Longitude
-114.02272°
Altitude
1,066.187 km
Speed
7.321 km/s
True Right ascension
20h 01m 28s
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
07:15:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.415 km
Perigee altitude
1,054.721 km
Semi-major axis
7,443.705 km
Eccentricity
0.00146
Inclination
88.9714°
RAAN
300.3669°
Arg. of periapsis
299.171°
True anomaly
60.94419°
Mean anomaly
60.7983°
Eccentric anomaly
60.87123°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00016519
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Other satellites on launch #46 in the year 2025 (2025-03-11 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.QIANFAN-89 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-20 20:58:48.019Z | 359.902° N | 2026-06-20 21:04:48.019Z | 207.775° SW | 44.734° | 2026-06-20 21:10:48.019Z | 184.45° SSW |
| 12 mins | 2026-06-21 08:55:48.019Z | 173.42° S | 2026-06-21 09:01:48.019Z | 29.903° NE | 44.252° | 2026-06-21 09:07:48.019Z | 0.973° NNE |
| 5 mins | 2026-06-21 10:46:48.019Z | 266.863° W | 2026-06-21 10:48:48.019Z | 286.749° WNW | 14.389° | 2026-06-21 10:51:48.019Z | 314.912° NW |
| 11 mins | 2026-06-21 20:05:48.019Z | 20.589° NNE | 2026-06-21 20:10:48.019Z | 83.005° E | 32.925° | 2026-06-21 20:16:48.019Z | 151.88° SSE |
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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