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, 1.2 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 26141.90492903 .00000106 00000-0 14561-3 0 9995
2 62790 88.9710 86.4313 0013560 237.7269 122.2569 13.51007838 68855Epoch: 2026-05-21T21:43Z
TLE epoch observation values (Epoch: 2026-05-21T21:43:05.868Z)
Latitude
0.00001°
Longitude
-118.88658°
Altitude
1,076.906 km
Speed
7.311 km/s
True Right ascension
05h 45m 43s
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
15:06:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.698 km
Perigee altitude
1,055.51 km
Semi-major axis
7,443.741 km
Eccentricity
0.00136
Inclination
88.971°
RAAN
86.4313°
Arg. of periapsis
237.7269°
True anomaly
122.38819°
Mean anomaly
122.2569°
Eccentric anomaly
122.32255°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00014561
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-22 07:13:15.037Z | 35.294° NE | 2026-05-22 07:17:15.037Z | 75.315° E | 19.258° | 2026-05-22 07:21:15.037Z | 117.256° SE |
| 11 mins | 2026-05-22 08:59:15.037Z | 351.508° N | 2026-05-22 09:04:15.037Z | 285.349° WNW | 41.472° | 2026-05-22 09:10:15.037Z | 197.91° SSW |
| 6 mins | 2026-05-22 19:13:15.037Z | 97.532° ESE | 2026-05-22 19:15:15.037Z | 76.683° E | 17.206° | 2026-05-22 19:19:15.037Z | 37.128° NE |
| 11 mins | 2026-05-22 20:56:15.037Z | 188.304° SSW | 2026-05-22 21:01:15.037Z | 262.339° W | 43.496° | 2026-05-22 21:07:15.037Z | 353.911° 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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