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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-60
1 62790U 25016F 26035.77257823 .00000102 00000-0 13977-3 0 9998
2 62790 88.9717 97.4854 0016212 180.2064 179.9083 13.50989664 54520Epoch: 2026-02-04T18:32Z
TLE epoch observation values (Epoch: 2026-02-04T18:32:30.759Z)
Latitude
-0.00002°
Longitude
44.42288°
Altitude
1,083.648 km
Speed
7.304 km/s
True Right ascension
06h 29m 56s
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
03:18:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.739 km
Perigee altitude
1,053.603 km
Semi-major axis
7,443.808 km
Eccentricity
0.00162
Inclination
88.9717°
RAAN
97.4854°
Arg. of periapsis
180.2064°
True anomaly
179.9086°
Mean anomaly
179.9083°
Eccentric anomaly
179.90845°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.00013977
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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 | 2026-02-05 03:32:22.600Z | 140.546° SSE | 2026-02-05 03:38:22.600Z | 71.278° E | 29.778° | 2026-02-05 03:43:22.600Z | 18.744° NNE |
| 11 mins | 2026-02-05 05:19:22.600Z | 215.779° SW | 2026-02-05 05:24:22.600Z | 276.565° WNW | 30.909° | 2026-02-05 05:30:22.600Z | 342.226° N |
| 6 mins | 2026-02-05 14:44:22.600Z | 53.1° ENE | 2026-02-05 14:46:22.600Z | 73.562° E | 15.645° | 2026-02-05 14:50:22.600Z | 111.94° ESE |
| 11 mins | 2026-02-05 16:28:22.600Z | 356.548° N | 2026-02-05 16:33:22.600Z | 309.104° NW | 43.708° | 2026-02-05 16:39:22.600Z | 190.283° SSW |
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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