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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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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-63
1 62793U 25016J 26305.79234514 .00000101 00000-0 13694-3 0 9990
2 62793 88.9730 69.4062 0017667 129.8808 230.3900 13.51034572 91024Epoch: 2026-11-01T19:00Z
TLE epoch observation values (Epoch: 2026-11-01T19:00:58.620Z)
Latitude
-0°
Longitude
103.08332°
Altitude
1,079.811 km
Speed
7.308 km/s
True Right ascension
04h 37m 37s
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
22:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.656 km
Perigee altitude
1,052.355 km
Semi-major axis
7,443.643 km
Eccentricity
0.00177
Inclination
88.973°
RAAN
69.4062°
Arg. of periapsis
129.8808°
True anomaly
230.23425°
Mean anomaly
230.39°
Eccentric anomaly
230.3121°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00013694
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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 | 2026-11-02 07:35:37.556Z | 121.558° SE | 2026-11-02 07:39:37.556Z | 79.497° E | 24.439° | 2026-11-02 07:44:37.556Z | 27.189° NE |
| 11 mins | 2026-11-02 09:20:37.556Z | 200.284° SSW | 2026-11-02 09:25:37.556Z | 262.286° W | 52.365° | 2026-11-02 09:31:37.556Z | 347.222° N |
| 11 mins | 2026-11-02 20:30:37.556Z | 6.035° NNE | 2026-11-02 20:35:37.556Z | 103.313° ESE | 76.083° | 2026-11-02 20:41:37.556Z | 175.955° S |
| 6 mins | 2026-11-02 22:18:37.556Z | 313.789° NW | 2026-11-02 22:21:37.556Z | 283.182° WNW | 16.359° | 2026-11-02 22:24:37.556Z | 254.66° W |
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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