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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-71
1 62801U 25016S 25286.93988986 .00000074 00000-0 96503-4 0 9992
2 62801 88.9730 109.2712 0016337 155.7384 204.4540 13.50972145 39164Epoch: 2025-10-13T22:33Z
TLE epoch observation values (Epoch: 2025-10-13T22:33:26.483Z)
Latitude
-0.00003°
Longitude
108.17538°
Altitude
1,082.717 km
Speed
7.305 km/s
True Right ascension
07h 17m 05s
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
10:48:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.896 km
Perigee altitude
1,053.574 km
Semi-major axis
7,443.872 km
Eccentricity
0.00163
Inclination
88.973°
RAAN
109.2712°
Arg. of periapsis
155.7384°
True anomaly
204.37665°
Mean anomaly
204.454°
Eccentric anomaly
204.41531°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000096503
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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 | 2025-10-15 00:01:41.284Z | 10.451° NNE | 2025-10-15 00:07:41.284Z | 75.95° E | 38.549° | 2025-10-15 00:13:41.284Z | 161.424° S |
| 8 mins | 2025-10-15 01:50:41.284Z | 323.223° NNW | 2025-10-15 01:53:41.284Z | 289.717° WNW | 21.874° | 2025-10-15 01:58:41.284Z | 236.576° WSW |
| 10 mins | 2025-10-15 12:00:41.284Z | 146.225° SSE | 2025-10-15 12:04:41.284Z | 94.573° ESE | 35.797° | 2025-10-15 12:10:41.284Z | 13.511° NNE |
| 9 mins | 2025-10-15 13:47:41.284Z | 230.948° WSW | 2025-10-15 13:51:41.284Z | 276.294° WNW | 24.705° | 2025-10-15 13:56:41.284Z | 331.784° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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