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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-65
1 62795U 25016L 26035.79736075 .00000107 00000-0 14768-3 0 9990
2 62795 88.9720 97.4679 0014384 178.9584 181.1599 13.50989050 54541Epoch: 2026-02-04T19:08Z
TLE epoch observation values (Epoch: 2026-02-04T19:08:11.968Z)
Latitude
-0.0001°
Longitude
35.45925°
Altitude
1,082.286 km
Speed
7.306 km/s
True Right ascension
06h 29m 52s
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
03:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.38 km
Perigee altitude
1,054.966 km
Semi-major axis
7,443.81 km
Eccentricity
0.00144
Inclination
88.972°
RAAN
97.4679°
Arg. of periapsis
178.9584°
True anomaly
181.15657°
Mean anomaly
181.1599°
Eccentric anomaly
181.15823°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.00014768
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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 | 2026-02-05 04:06:58.901Z | 165.016° S | 2026-02-05 04:12:58.901Z | 103.883° ESE | 42.131° | 2026-02-05 04:18:58.901Z | 6.481° NNE |
| 8 mins | 2026-02-05 05:56:58.901Z | 247.121° WSW | 2026-02-05 05:59:58.901Z | 277.623° WNW | 18.358° | 2026-02-05 06:04:58.901Z | 326.731° NNW |
| 10 mins | 2026-02-05 15:17:58.901Z | 26.679° NE | 2026-02-05 15:22:58.901Z | 87.122° E | 27.396° | 2026-02-05 15:27:58.901Z | 140.814° SSE |
| 10 mins | 2026-02-05 17:04:58.901Z | 337.978° N | 2026-02-05 17:08:58.901Z | 285.41° WNW | 32.811° | 2026-02-05 17:14:58.901Z | 213.664° 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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