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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-64
1 62794U 25016K 26077.57322051 .00000014 00000-0 23362-5 0 9995
2 62794 88.9668 93.0960 0016059 68.4095 291.8766 13.51006078 60203Epoch: 2026-03-18T13:45Z
TLE epoch observation values (Epoch: 2026-03-18T13:45:26.252Z)
Latitude
0.00005°
Longitude
70.60157°
Altitude
1,067.072 km
Speed
7.321 km/s
True Right ascension
06h 12m 23s
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
00:24:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.564 km
Perigee altitude
1,053.657 km
Semi-major axis
7,443.747 km
Eccentricity
0.00161
Inclination
88.9668°
RAAN
93.096°
Arg. of periapsis
68.4095°
True anomaly
291.7057°
Mean anomaly
291.8766°
Eccentric anomaly
291.79116°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.0000023362
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-03-19 00:31:56.904Z | 141.58° SSE | 2026-03-19 00:36:56.904Z | 88.836° E | 30.242° | 2026-03-19 00:42:56.904Z | 17.669° NNE |
| 9 mins | 2026-03-19 02:19:56.904Z | 223.74° SW | 2026-03-19 02:23:56.904Z | 277.906° WNW | 29.789° | 2026-03-19 02:28:56.904Z | 337.214° NNW |
| 6 mins | 2026-03-19 11:43:56.904Z | 54.196° ENE | 2026-03-19 11:45:56.904Z | 75.186° E | 16.369° | 2026-03-19 11:49:56.904Z | 113.726° SE |
| 11 mins | 2026-03-19 13:27:56.904Z | 355.477° N | 2026-03-19 13:32:56.904Z | 294.53° NW | 43.611° | 2026-03-19 13:38:56.904Z | 191.624° 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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