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: 1 day ago
TLE from 1 day ago
0 QIANFAN-69
1 62799U 25016Q 25306.48074735 .00000081 00000-0 10615-3 0 9996
2 62799 88.9721 107.1358 0017510 100.8581 259.4541 13.50970718 41840Epoch: 2025-11-02T11:32Z
TLE epoch observation values (Epoch: 2025-11-02T11:32:16.571Z)
Latitude
-0.00007°
Longitude
-107.92911°
Altitude
1,074.051 km
Speed
7.314 km/s
True Right ascension
07h 08m 32s
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
14:39:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.775 km
Perigee altitude
1,052.706 km
Semi-major axis
7,443.877 km
Eccentricity
0.00175
Inclination
88.9721°
RAAN
107.1358°
Arg. of periapsis
100.8581°
True anomaly
259.25692°
Mean anomaly
259.4541°
Eccentric anomaly
259.3555°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00010615
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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 | 2025-11-03 21:54:29.991Z | 25.761° NE | 2025-11-03 21:59:29.991Z | 76.267° E | 23.55° | 2025-11-03 22:04:29.991Z | 131.232° SE |
| 11 mins | 2025-11-03 23:41:29.991Z | 345.7° N | 2025-11-03 23:46:29.991Z | 278.829° WNW | 36.94° | 2025-11-03 23:52:29.991Z | 206.285° SW |
| 8 mins | 2025-11-04 09:54:29.991Z | 111.561° ESE | 2025-11-04 09:57:29.991Z | 77.778° E | 21.206° | 2025-11-04 10:02:29.991Z | 27.24° NE |
| 11 mins | 2025-11-04 11:38:29.991Z | 198.295° SSW | 2025-11-04 11:43:29.991Z | 264.953° W | 39.56° | 2025-11-04 11:49:29.991Z | 348.842° 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
Authenticating...
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