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: 1 day ago
TLE from 1 day ago
0 QIANFAN-63
1 62793U 25016J 25306.47654079 .00000076 00000-0 98130-4 0 9997
2 62793 88.9746 107.2157 0017831 104.0917 256.2217 13.50973443 41836Epoch: 2025-11-02T11:26Z
TLE epoch observation values (Epoch: 2025-11-02T11:26:13.124Z)
Latitude
-0.00004°
Longitude
-106.3307°
Altitude
1,074.818 km
Speed
7.313 km/s
True Right ascension
07h 08m 51s
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
14:37:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.004 km
Perigee altitude
1,052.457 km
Semi-major axis
7,443.867 km
Eccentricity
0.00178
Inclination
88.9746°
RAAN
107.2157°
Arg. of periapsis
104.0917°
True anomaly
256.02336°
Mean anomaly
256.2217°
Eccentric anomaly
256.12252°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00009813
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-03 21:49:21.819Z | 33.429° NE | 2025-11-03 21:53:21.819Z | 75.378° E | 21.367° | 2025-11-03 21:58:21.819Z | 127.701° SE |
| 11 mins | 2025-11-03 23:35:21.819Z | 348.537° N | 2025-11-03 23:40:21.819Z | 282.228° WNW | 39.161° | 2025-11-03 23:46:21.819Z | 202.545° SW |
| 7 mins | 2025-11-04 09:48:21.819Z | 109.915° ESE | 2025-11-04 09:51:21.819Z | 78.604° E | 19.134° | 2025-11-04 09:55:21.819Z | 36.312° NE |
| 11 mins | 2025-11-04 11:32:21.819Z | 193.48° SSW | 2025-11-04 11:37:21.819Z | 258.906° W | 41.484° | 2025-11-04 11:43:21.819Z | 350.94° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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