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, 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-69
1 62799U 25016Q 25256.93117368 .00000066 00000-0 83231-4 0 9998
2 62799 88.9752 112.2715 0014048 242.8929 117.0790 13.50965212 35159Epoch: 2025-09-13T22:20Z
TLE epoch observation values (Epoch: 2025-09-13T22:20:53.405Z)
Latitude
-0.00001°
Longitude
143.89152°
Altitude
1,076.437 km
Speed
7.311 km/s
True Right ascension
07h 29m 05s
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
00:22:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.218 km
Perigee altitude
1,055.303 km
Semi-major axis
7,443.898 km
Eccentricity
0.0014
Inclination
88.9752°
RAAN
112.2715°
Arg. of periapsis
242.8929°
True anomaly
117.22222°
Mean anomaly
117.079°
Eccentric anomaly
117.15062°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.000083231
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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 | 2025-09-14 14:26:49.667Z | 160.352° S | 2025-09-14 14:32:49.667Z | 78.528° E | 40.755° | 2025-09-14 14:38:49.667Z | 7.554° NNE |
| 8 mins | 2025-09-14 16:15:49.667Z | 241.146° WSW | 2025-09-14 16:19:49.667Z | 283.848° WNW | 20.296° | 2025-09-14 16:23:49.667Z | 324.827° NNW |
| 9 mins | 2025-09-15 01:37:49.667Z | 31.724° NE | 2025-09-15 01:41:49.667Z | 78.144° E | 25.534° | 2025-09-15 01:46:49.667Z | 134.549° SE |
| 11 mins | 2025-09-15 03:23:49.667Z | 343.099° N | 2025-09-15 03:28:49.667Z | 275.202° WNW | 35.189° | 2025-09-15 03:34:49.667Z | 208.865° SW |
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
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