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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-71
1 62801U 25016S 25341.89578576 .00000177 00000-0 25541-3 0 9996
2 62801 88.9766 103.5871 0015459 8.7387 351.4030 13.50982660 46584Epoch: 2025-12-07T21:29Z
TLE epoch observation values (Epoch: 2025-12-07T21:29:55.889Z)
Latitude
-0.00007°
Longitude
64.20162°
Altitude
1,060.214 km
Speed
7.327 km/s
True Right ascension
06h 54m 20s
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
05:19:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.204 km
Perigee altitude
1,054.189 km
Semi-major axis
7,443.833 km
Eccentricity
0.00155
Inclination
88.9766°
RAAN
103.5871°
Arg. of periapsis
8.7387°
True anomaly
351.37647°
Mean anomaly
351.403°
Eccentric anomaly
351.38974°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00025541
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-08 08:15:43.496Z | 159.266° S | 2025-12-08 08:21:43.496Z | 83.306° E | 39.958° | 2025-12-08 08:27:43.496Z | 8.468° NNE |
| 7 mins | 2025-12-08 10:05:43.496Z | 247.712° W | 2025-12-08 10:08:43.496Z | 282.469° WNW | 20.696° | 2025-12-08 10:12:43.496Z | 324.758° NNW |
| 9 mins | 2025-12-08 19:26:43.496Z | 32.268° NE | 2025-12-08 19:30:43.496Z | 77.729° E | 24.802° | 2025-12-08 19:35:43.496Z | 133.099° SE |
| 11 mins | 2025-12-08 21:12:43.496Z | 344.139° N | 2025-12-08 21:17:43.496Z | 275.897° WNW | 36.136° | 2025-12-08 21:23:43.496Z | 207.662° SW |
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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