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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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, 1.2 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-60
1 62790U 25016F 25306.48899514 .00000070 00000-0 88877-4 0 9991
2 62790 88.9726 107.2399 0017482 99.4201 260.8928 13.50973202 41792Epoch: 2025-11-02T11:44Z
TLE epoch observation values (Epoch: 2025-11-02T11:44:09.180Z)
Latitude
0.00007°
Longitude
-110.80234°
Altitude
1,073.716 km
Speed
7.314 km/s
True Right ascension
07h 08m 57s
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
14:41:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.745 km
Perigee altitude
1,052.718 km
Semi-major axis
7,443.868 km
Eccentricity
0.00175
Inclination
88.9726°
RAAN
107.2399°
Arg. of periapsis
99.4201°
True anomaly
260.69507°
Mean anomaly
260.8928°
Eccentric anomaly
260.79393°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000088877
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-03 22:06:51.919Z | 25.311° NE | 2025-11-03 22:11:51.919Z | 84.121° E | 27.733° | 2025-11-03 22:16:51.919Z | 140.223° SSE |
| 10 mins | 2025-11-03 23:53:51.919Z | 338.749° N | 2025-11-03 23:57:51.919Z | 289.175° WNW | 32.353° | 2025-11-04 00:03:51.919Z | 214.821° SW |
| 8 mins | 2025-11-04 10:05:51.919Z | 120.66° SE | 2025-11-04 10:09:51.919Z | 70.218° E | 24.937° | 2025-11-04 10:13:51.919Z | 27.109° NE |
| 11 mins | 2025-11-04 11:50:51.919Z | 208.407° SW | 2025-11-04 11:55:51.919Z | 280.661° WNW | 35.415° | 2025-11-04 12:01:51.919Z | 346.664° 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
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