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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-64
1 62794U 25016K 25351.84505459 .00000132 00000-0 18613-3 0 9996
2 62794 88.9769 102.5058 0012806 331.6784 28.3669 13.50980057 47954Epoch: 2025-12-17T20:16Z
TLE epoch observation values (Epoch: 2025-12-17T20:16:52.716Z)
Latitude
-0.00009°
Longitude
71.57707°
Altitude
1,063.218 km
Speed
7.324 km/s
True Right ascension
06h 50m 01s
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
10:16:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.239 km
Perigee altitude
1,056.173 km
Semi-major axis
7,443.843 km
Eccentricity
0.00128
Inclination
88.9769°
RAAN
102.5058°
Arg. of periapsis
331.6784°
True anomaly
28.43672°
Mean anomaly
28.3669°
Eccentric anomaly
28.4018°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00018613
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-18 18:14:20.819Z | 44.446° NE | 2025-12-18 18:17:20.819Z | 73.217° E | 15.483° | 2025-12-18 18:21:20.819Z | 110.987° ESE |
| 12 mins | 2025-12-18 19:59:20.819Z | 357.264° N | 2025-12-18 20:04:20.819Z | 316.224° NNW | 43.897° | 2025-12-18 20:11:20.819Z | 188.465° SSW |
| 4 mins | 2025-12-19 06:14:20.819Z | 88.037° E | 2025-12-19 06:16:20.819Z | 68.681° E | 13.43° | 2025-12-19 06:18:20.819Z | 49.73° ENE |
| 11 mins | 2025-12-19 07:56:20.819Z | 178.155° S | 2025-12-19 08:01:20.819Z | 188.277° SSW | 44.685° | 2025-12-19 08:07:20.819Z | 358.657° N |
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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