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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-71
1 62801U 25016S 26035.77667028 .00000108 00000-0 14824-3 0 9991
2 62801 88.9727 97.5020 0015967 185.1515 174.9474 13.50993579 54531Epoch: 2026-02-04T18:38Z
TLE epoch observation values (Epoch: 2026-02-04T18:38:24.312Z)
Latitude
-0.00005°
Longitude
42.96231°
Altitude
1,083.405 km
Speed
7.305 km/s
True Right ascension
06h 30m 00s
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
03:17:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.542 km
Perigee altitude
1,053.771 km
Semi-major axis
7,443.793 km
Eccentricity
0.0016
Inclination
88.9727°
RAAN
97.502°
Arg. of periapsis
185.1515°
True anomaly
174.96348°
Mean anomaly
174.9474°
Eccentric anomaly
174.95544°
Mean motion
3.37949 °/min
Orbital period
106.52 mins
BSTAR
0.00014824
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-05 03:37:49.555Z | 145.527° SSE | 2026-02-05 03:43:49.555Z | 79.19° E | 32.174° | 2026-02-05 03:48:49.555Z | 18.872° NNE |
| 10 mins | 2026-02-05 05:25:49.555Z | 222.558° SW | 2026-02-05 05:29:49.555Z | 269.118° W | 28.502° | 2026-02-05 05:35:49.555Z | 338.478° N |
| 7 mins | 2026-02-05 14:49:49.555Z | 47.893° ENE | 2026-02-05 14:52:49.555Z | 79.817° E | 17.355° | 2026-02-05 14:56:49.555Z | 118.081° SE |
| 11 mins | 2026-02-05 16:34:49.555Z | 353.148° N | 2026-02-05 16:39:49.555Z | 265.439° W | 42.934° | 2026-02-05 16:45:49.555Z | 193.576° SSW |
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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