QIANFAN-69, 62799
Orbit data source: Space-Track
QIANFAN-69, 62799 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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62799 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-69
1 62799U 25016Q 25352.54872720 .00000141 00000-0 19960-3 0 9993
2 62799 88.9758 102.3688 0014547 332.7451 27.2936 13.50988097 48061Epoch: 2025-12-18T13:10Z
TLE epoch observation values (Epoch: 2025-12-18T13:10:10.030Z)
Latitude
0.00008°
Longitude
177.42436°
Altitude
1,061.953 km
Speed
7.326 km/s
True Right ascension
06h 49m 28s
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
21:01:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.505 km
Perigee altitude
1,054.848 km
Semi-major axis
7,443.814 km
Eccentricity
0.00145
Inclination
88.9758°
RAAN
102.3688°
Arg. of periapsis
332.7451°
True anomaly
27.37016°
Mean anomaly
27.2936°
Eccentric anomaly
27.33187°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.0001996
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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-69 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-19 07:03:50.510Z | 139.29° SSE | 2025-12-19 07:08:50.510Z | 78.302° E | 30.847° | 2025-12-19 07:13:50.510Z | 19.598° NNE |
| 10 mins | 2025-12-19 08:50:50.510Z | 220.995° SW | 2025-12-19 08:54:50.510Z | 269.49° W | 29.476° | 2025-12-19 09:00:50.510Z | 339.71° N |
| 6 mins | 2025-12-19 18:14:50.510Z | 48.777° ENE | 2025-12-19 18:17:50.510Z | 79.846° E | 16.778° | 2025-12-19 18:20:50.510Z | 109.365° ESE |
| 11 mins | 2025-12-19 19:59:50.510Z | 354.527° N | 2025-12-19 20:04:50.510Z | 262.854° W | 43.62° | 2025-12-19 20:10:50.510Z | 191.677° 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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