QIANFAN-74, 63160
Orbit data source: Space-Track
QIANFAN-74, 63160 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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63160 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, 1.7 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-74
1 63160U 25046B 26171.41321825 .00000121 00000-0 16900-3 0 9999
2 63160 88.9713 300.2374 0002182 110.2168 249.9218 13.51009915 73082Epoch: 2026-06-20T09:55Z
TLE epoch observation values (Epoch: 2026-06-20T09:55:02.056Z)
Latitude
-0.00003°
Longitude
-117.14937°
Altitude
1,072.057 km
Speed
7.316 km/s
True Right ascension
20h 00m 56s
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
10:19:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.221 km
Perigee altitude
1,063.972 km
Semi-major axis
7,443.733 km
Eccentricity
0.00022
Inclination
88.9713°
RAAN
300.2374°
Arg. of periapsis
110.2168°
True anomaly
249.89832°
Mean anomaly
249.9218°
Eccentric anomaly
249.91006°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.000169
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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-74 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 07:24:25.408Z | 102.179° ESE | 2026-06-21 07:27:25.408Z | 73.719° E | 15.085° | 2026-06-21 07:30:25.408Z | 44.394° NE |
| 11 mins | 2026-06-21 09:08:25.408Z | 183.202° SSW | 2026-06-21 09:13:25.408Z | 289.584° WNW | 44.55° | 2026-06-21 09:19:25.408Z | 356.732° N |
| 10 mins | 2026-06-21 20:18:25.408Z | 19.171° NNE | 2026-06-21 20:22:25.408Z | 75.057° E | 37.217° | 2026-06-21 20:28:25.408Z | 158.622° S |
| 8 mins | 2026-06-21 22:05:25.408Z | 324.845° NNW | 2026-06-21 22:09:25.408Z | 276.815° WNW | 23.285° | 2026-06-21 22:13:25.408Z | 235.346° 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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