QIANFAN-63, 62793
Orbit data source: Space-Track
QIANFAN-63, 62793 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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62793 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, 1.2 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-63
1 62793U 25016J 25352.54456963 .00000144 00000-0 20465-3 0 9999
2 62793 88.9783 102.4603 0014968 336.4146 23.6317 13.50985221 48058Epoch: 2025-12-18T13:04Z
TLE epoch observation values (Epoch: 2025-12-18T13:04:10.816Z)
Latitude
-0.00002°
Longitude
179.01668°
Altitude
1,061.378 km
Speed
7.326 km/s
True Right ascension
06h 49m 50s
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
20:56:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.829 km
Perigee altitude
1,054.545 km
Semi-major axis
7,443.824 km
Eccentricity
0.0015
Inclination
88.9783°
RAAN
102.4603°
Arg. of periapsis
336.4146°
True anomaly
23.70057°
Mean anomaly
23.6317°
Eccentric anomaly
23.66612°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00020465
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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-63 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 | 2025-12-19 06:57:29.719Z | 137.614° SSE | 2025-12-19 07:02:29.719Z | 84.881° E | 28.332° | 2025-12-19 07:08:29.719Z | 18.602° NNE |
| 10 mins | 2025-12-19 08:44:29.719Z | 214.859° SW | 2025-12-19 08:49:29.719Z | 281.669° WNW | 31.978° | 2025-12-19 08:54:29.719Z | 339.997° N |
| 5 mins | 2025-12-19 18:09:29.719Z | 55.74° ENE | 2025-12-19 18:11:29.719Z | 75.786° E | 14.997° | 2025-12-19 18:14:29.719Z | 104.481° ESE |
| 11 mins | 2025-12-19 19:53:29.719Z | 357.883° N | 2025-12-19 19:58:29.719Z | 302.807° NW | 44.504° | 2025-12-19 20:04:29.719Z | 187.682° 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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