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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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, 5.0 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 25256.90436783 .00000069 00000-0 85869-4 0 9997
2 62794 88.9764 112.3299 0012209 237.3705 122.6269 13.52420311 35132Epoch: 2025-09-13T21:42Z
TLE epoch observation values (Epoch: 2025-09-13T21:42:17.38Z)
Latitude
-0.00005°
Longitude
153.62645°
Altitude
1,071.23 km
Speed
7.314 km/s
True Right ascension
07h 29m 19s
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
00:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,069.498 km
Perigee altitude
1,051.334 km
Semi-major axis
7,438.553 km
Eccentricity
0.00122
Inclination
88.9764°
RAAN
112.3299°
Arg. of periapsis
237.3705°
True anomaly
122.74463°
Mean anomaly
122.6269°
Eccentric anomaly
122.68578°
Mean motion
3.38307 °/min
Orbital period
106.41 mins
BSTAR
0.000085869
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-14 13:48:49.134Z | 129.576° SE | 2025-09-14 13:53:49.134Z | 71.069° E | 26.115° | 2025-09-14 13:58:49.134Z | 21.191° NNE |
| 11 mins | 2025-09-14 15:34:49.134Z | 210.428° SW | 2025-09-14 15:39:49.134Z | 281.337° WNW | 34.557° | 2025-09-14 15:45:49.134Z | 345.944° N |
| 4 mins | 2025-09-15 00:59:49.134Z | 61.5° ENE | 2025-09-15 01:00:49.134Z | 71.083° E | 12.796° | 2025-09-15 01:03:49.134Z | 98.914° ESE |
| 12 mins | 2025-09-15 02:42:49.134Z | 0.972° NNE | 2025-09-15 02:48:49.134Z | 180.735° SSW | 44.602° | 2025-09-15 02:54:49.134Z | 182.699° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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