QIANFAN-64, 62794
Orbit data source: Space-Track
QIANFAN-64, 62794 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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62794 intel report (Beta)
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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-64
1 62794U 25016K 26092.23766142 .00000031 00000-0 28909-4 0 9998
2 62794 88.9667 91.5665 0015105 30.1256 330.0761 13.51006631 62188Epoch: 2026-04-02T05:42Z
TLE epoch observation values (Epoch: 2026-04-02T05:42:13.946Z)
Latitude
-0.00001°
Longitude
175.41937°
Altitude
1,061.764 km
Speed
7.326 km/s
True Right ascension
06h 06m 15s
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
21:25:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.852 km
Perigee altitude
1,054.365 km
Semi-major axis
7,443.745 km
Eccentricity
0.00151
Inclination
88.9667°
RAAN
91.5665°
Arg. of periapsis
30.1256°
True anomaly
329.98961°
Mean anomaly
330.0761°
Eccentric anomaly
330.03287°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000028909
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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-64 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 | 2026-04-02 23:34:44.000Z | 148.764° SSE | 2026-04-02 23:40:44.000Z | 80.974° E | 33.777° | 2026-04-02 23:46:44.000Z | 13.533° NNE |
| 9 mins | 2026-04-03 01:23:44.000Z | 231.904° WSW | 2026-04-03 01:27:44.000Z | 284.58° WNW | 26.444° | 2026-04-03 01:32:44.000Z | 336.719° NNW |
| 7 mins | 2026-04-03 10:46:44.000Z | 46.493° ENE | 2026-04-03 10:49:44.000Z | 79.51° E | 19.112° | 2026-04-03 10:53:44.000Z | 119.577° SE |
| 11 mins | 2026-04-03 12:31:44.000Z | 350.922° N | 2026-04-03 12:36:44.000Z | 269.342° W | 41.736° | 2026-04-03 12:42:44.000Z | 196.854° 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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