QIANFAN-71, 62801
Orbit data source: Space-Track
QIANFAN-71, 62801 is a Chinese payload satellite in LEO that was launched on Thu, 23 Jan 2025 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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62801 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-71
1 62801U 25016S 26092.28710605 .00000046 00000-0 52535-4 0 9993
2 62801 88.9671 91.6195 0016971 35.8288 324.3998 13.51008143 62166Epoch: 2026-04-02T06:53Z
TLE epoch observation values (Epoch: 2026-04-02T06:53:25.962Z)
Latitude
-0.00003°
Longitude
157.62357°
Altitude
1,061.234 km
Speed
7.326 km/s
True Right ascension
06h 06m 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
21:21:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.236 km
Perigee altitude
1,052.97 km
Semi-major axis
7,443.74 km
Eccentricity
0.0017
Inclination
88.9671°
RAAN
91.6195°
Arg. of periapsis
35.8288°
True anomaly
324.2864°
Mean anomaly
324.3998°
Eccentric anomaly
324.34312°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000052535
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Other satellites on launch #16 in the year 2025 (2025-01-23 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-71 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-02 23:01:49.135Z | 116.686° SE | 2026-04-02 23:05:49.135Z | 73.512° E | 20.851° | 2026-04-02 23:09:49.135Z | 31.839° NE |
| 11 mins | 2026-04-03 00:46:49.135Z | 198.775° SSW | 2026-04-03 00:51:49.135Z | 276.941° WNW | 39.87° | 2026-04-03 00:57:49.135Z | 350.048° N |
| 12 mins | 2026-04-03 11:55:49.135Z | 6.988° NNE | 2026-04-03 12:00:49.135Z | 63.224° ENE | 43.088° | 2026-04-03 12:07:49.135Z | 173.752° S |
| 6 mins | 2026-04-03 13:44:49.135Z | 310.349° NW | 2026-04-03 13:46:49.135Z | 289.162° WNW | 17.219° | 2026-04-03 13:50:49.135Z | 249.982° W |
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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