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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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-69
1 62799U 25016Q 26257.58199395 .00000027 00000-0 23081-4 0 9995
2 62799 88.9644 74.2640 0013946 268.0607 91.8947 13.51024044 84520Epoch: 2026-09-14T13:58Z
TLE epoch observation values (Epoch: 2026-09-14T13:58:04.277Z)
Latitude
-0.00001°
Longitude
-128.81405°
Altitude
1,071.804 km
Speed
7.316 km/s
True Right ascension
04h 57m 03s
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
14:59:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.925 km
Perigee altitude
1,055.163 km
Semi-major axis
7,443.681 km
Eccentricity
0.00139
Inclination
88.9644°
RAAN
74.264°
Arg. of periapsis
268.0607°
True anomaly
92.05441°
Mean anomaly
91.8947°
Eccentric anomaly
91.97456°
Mean motion
3.37957 °/min
Orbital period
106.52 mins
BSTAR
0.000023081
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-14 23:26:54.796Z | 16.354° NNE | 2026-09-14 23:32:54.796Z | 86.906° E | 41.493° | 2026-09-14 23:38:54.796Z | 153.476° SSE |
| 9 mins | 2026-09-15 01:14:54.796Z | 332.512° NNW | 2026-09-15 01:18:54.796Z | 285.277° WNW | 31.261° | 2026-09-15 01:23:54.796Z | 227.428° WSW |
| 10 mins | 2026-09-15 11:25:54.796Z | 133.261° SE | 2026-09-15 11:29:54.796Z | 80.613° E | 36.311° | 2026-09-15 11:35:54.796Z | 16.217° NNE |
| 10 mins | 2026-09-15 13:11:54.796Z | 219.688° SW | 2026-09-15 13:16:54.796Z | 285.908° WNW | 35.367° | 2026-09-15 13:21:54.796Z | 339.4° 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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