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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-63
1 62793U 25016J 26257.57801176 .00000024 00000-0 19205-4 0 9995
2 62793 88.9669 74.4225 0014280 272.1123 87.8393 13.51022740 84513Epoch: 2026-09-14T13:52Z
TLE epoch observation values (Epoch: 2026-09-14T13:52:20.216Z)
Latitude
0.00001°
Longitude
-127.21803°
Altitude
1,071.065 km
Speed
7.317 km/s
True Right ascension
04h 57m 41s
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
14:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.179 km
Perigee altitude
1,054.92 km
Semi-major axis
7,443.686 km
Eccentricity
0.00143
Inclination
88.9669°
RAAN
74.4225°
Arg. of periapsis
272.1123°
True anomaly
88.00283°
Mean anomaly
87.8393°
Eccentric anomaly
87.92106°
Mean motion
3.37957 °/min
Orbital period
106.52 mins
BSTAR
0.000019205
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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 | 2026-09-14 23:21:48.081Z | 21.219° NNE | 2026-09-14 23:26:48.081Z | 78.917° E | 37.046° | 2026-09-14 23:32:48.081Z | 148.258° SSE |
| 10 mins | 2026-09-15 01:08:48.081Z | 337.118° NNW | 2026-09-15 01:13:48.081Z | 274.514° WNW | 34.753° | 2026-09-15 01:18:48.081Z | 220.773° SW |
| 10 mins | 2026-09-15 11:19:48.081Z | 132.132° SE | 2026-09-15 11:24:48.081Z | 70.024° E | 32.187° | 2026-09-15 11:29:48.081Z | 19.659° NNE |
| 11 mins | 2026-09-15 13:05:48.081Z | 213.509° SW | 2026-09-15 13:10:48.081Z | 278.969° WNW | 39.916° | 2026-09-15 13:16:48.081Z | 344.019° 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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