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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-60
1 62790U 25016F 25356.77866299 .00000067 00000-0 85195-4 0 9998
2 62790 88.9762 102.0387 0014184 317.5769 42.4285 13.50986302 48580Epoch: 2025-12-22T18:41Z
TLE epoch observation values (Epoch: 2025-12-22T18:41:16.482Z)
Latitude
0.00002°
Longitude
90.14815°
Altitude
1,063.794 km
Speed
7.324 km/s
True Right ascension
06h 48m 09s
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
05:37:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.241 km
Perigee altitude
1,055.125 km
Semi-major axis
7,443.82 km
Eccentricity
0.00142
Inclination
88.9762°
RAAN
102.0387°
Arg. of periapsis
317.5769°
True anomaly
42.5383°
Mean anomaly
42.4285°
Eccentric anomaly
42.48339°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.000085195
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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 | 2025-12-23 07:13:54.628Z | 160.907° S | 2025-12-23 07:19:54.628Z | 75.761° E | 40.942° | 2025-12-23 07:25:54.628Z | 7.104° NNE |
| 8 mins | 2025-12-23 09:02:54.628Z | 241.935° WSW | 2025-12-23 09:06:54.628Z | 284.609° WNW | 19.792° | 2025-12-23 09:10:54.628Z | 325.113° NNW |
| 9 mins | 2025-12-23 18:24:54.628Z | 32.075° NE | 2025-12-23 18:28:54.628Z | 79.395° E | 26.028° | 2025-12-23 18:33:54.628Z | 135.47° SSE |
| 11 mins | 2025-12-23 20:10:54.628Z | 342.306° N | 2025-12-23 20:15:54.628Z | 273.243° WNW | 34.895° | 2025-12-23 20:21:54.628Z | 209.207° SW |
| 7 mins | 2025-12-24 06:22:54.628Z | 119.11° SE | 2025-12-24 06:26:54.628Z | 72.697° E | 23.244° | 2025-12-24 06:29:54.628Z | 37.498° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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