QIANFAN-65, 62795
Orbit data source: Space-Track
QIANFAN-65, 62795 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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62795 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, 1.6 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-65
1 62795U 25016L 25306.43950950 .00000064 00000-0 80661-4 0 9999
2 62795 88.9729 107.2264 0015617 99.3197 260.9721 13.50974161 41801Epoch: 2025-11-02T10:32Z
TLE epoch observation values (Epoch: 2025-11-02T10:32:53.620Z)
Latitude
-0.00002°
Longitude
-92.95223°
Altitude
1,073.473 km
Speed
7.314 km/s
True Right ascension
07h 08m 54s
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
14:39:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.353 km
Perigee altitude
1,054.103 km
Semi-major axis
7,443.865 km
Eccentricity
0.00156
Inclination
88.9729°
RAAN
107.2264°
Arg. of periapsis
99.3197°
True anomaly
260.79541°
Mean anomaly
260.9721°
Eccentric anomaly
260.88375°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000080661
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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-65 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 | 2025-11-03 22:41:47.394Z | 10.493° NNE | 2025-11-03 22:47:47.394Z | 106.59° ESE | 40.441° | 2025-11-03 22:53:47.394Z | 167.47° S |
| 8 mins | 2025-11-04 00:29:47.394Z | 322.958° NNW | 2025-11-04 00:33:47.394Z | 279.071° WNW | 19.854° | 2025-11-04 00:37:47.394Z | 240.423° WSW |
| 10 mins | 2025-11-04 10:39:47.394Z | 151.772° SSE | 2025-11-04 10:44:47.394Z | 72.381° E | 38.123° | 2025-11-04 10:49:47.394Z | 11.909° NNE |
| 8 mins | 2025-11-04 12:27:47.394Z | 239.964° WSW | 2025-11-04 12:30:47.394Z | 273.667° WNW | 22.197° | 2025-11-04 12:35:47.394Z | 328.603° 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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