QIANFAN-60, 62790
Orbit data source: Space-Track
QIANFAN-60, 62790 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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62790 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-60
1 62790U 25016F 26257.59028015 .00000044 00000-0 49043-4 0 9992
2 62790 88.9648 74.3812 0013903 266.2665 93.6897 13.51027668 84477Epoch: 2026-09-14T14:10Z
TLE epoch observation values (Epoch: 2026-09-14T14:10:00.204Z)
Latitude
0.00001°
Longitude
-131.68804°
Altitude
1,072.114 km
Speed
7.316 km/s
True Right ascension
04h 57m 31s
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
14:59:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.88 km
Perigee altitude
1,055.182 km
Semi-major axis
7,443.668 km
Eccentricity
0.00139
Inclination
88.9648°
RAAN
74.3812°
Arg. of periapsis
266.2665°
True anomaly
93.84867°
Mean anomaly
93.6897°
Eccentric anomaly
93.76919°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.000049043
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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-60 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 23:38:24.005Z | 11.351° NNE | 2026-09-14 23:44:24.005Z | 74.879° E | 50.253° | 2026-09-14 23:50:24.005Z | 159.004° S |
| 8 mins | 2026-09-15 01:27:24.005Z | 324.523° NNW | 2026-09-15 01:30:24.005Z | 290.816° WNW | 25.453° | 2026-09-15 01:35:24.005Z | 235.712° WSW |
| 10 mins | 2026-09-15 11:37:24.005Z | 143.239° SSE | 2026-09-15 11:41:24.005Z | 90.826° ESE | 43.885° | 2026-09-15 11:47:24.005Z | 14.324° NNE |
| 9 mins | 2026-09-15 13:24:24.005Z | 230.114° WSW | 2026-09-15 13:28:24.005Z | 278.001° WNW | 29.291° | 2026-09-15 13:33:24.005Z | 333.478° NNW |
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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