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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-60
1 62790U 25016F 26051.91850896 .00000060 00000-0 73235-4 0 9998
2 62790 88.9690 95.8069 0017470 136.3133 223.9404 13.50991717 56707Epoch: 2026-02-20T22:02Z
TLE epoch observation values (Epoch: 2026-02-20T22:02:39.174Z)
Latitude
-0.00004°
Longitude
-25.70488°
Altitude
1,080.946 km
Speed
7.307 km/s
True Right ascension
06h 23m 13s
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
09:51:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.668 km
Perigee altitude
1,052.659 km
Semi-major axis
7,443.8 km
Eccentricity
0.00175
Inclination
88.969°
RAAN
95.8069°
Arg. of periapsis
136.3133°
True anomaly
223.8017°
Mean anomaly
223.9404°
Eccentric anomaly
223.87103°
Mean motion
3.37949 °/min
Orbital period
106.52 mins
BSTAR
0.000073235
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-21 14:38:28.029Z | 12.839° NNE | 2026-02-21 14:43:28.029Z | 72.058° E | 38.584° | 2026-02-21 14:49:28.029Z | 161.467° S |
| 8 mins | 2026-02-21 16:26:28.029Z | 323.989° NNW | 2026-02-21 16:30:28.029Z | 277.8° WNW | 21.593° | 2026-02-21 16:34:28.029Z | 237.56° WSW |
| 10 mins | 2026-02-22 02:36:28.029Z | 147.294° SSE | 2026-02-22 02:41:28.029Z | 71.621° E | 36.087° | 2026-02-22 02:46:28.029Z | 13.744° NNE |
| 9 mins | 2026-02-22 04:23:28.029Z | 230.311° WSW | 2026-02-22 04:27:28.029Z | 274.445° WNW | 24.378° | 2026-02-22 04:32:28.029Z | 330.822° 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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