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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-60
1 62790U 25016F 25352.55701895 .00000041 00000-0 44458-4 0 9999
2 62790 88.9762 102.4749 0014427 330.9639 29.0708 13.50985059 48018Epoch: 2025-12-18T13:22Z
TLE epoch observation values (Epoch: 2025-12-18T13:22:06.437Z)
Latitude
-0.00004°
Longitude
174.53726°
Altitude
1,062.201 km
Speed
7.325 km/s
True Right ascension
06h 49m 53s
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
20:57:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.427 km
Perigee altitude
1,054.948 km
Semi-major axis
7,443.825 km
Eccentricity
0.00144
Inclination
88.9762°
RAAN
102.4749°
Arg. of periapsis
330.9639°
True anomaly
29.15125°
Mean anomaly
29.0708°
Eccentric anomaly
29.11101°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.000044458
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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 | 2025-12-19 07:15:26.318Z | 147.853° SSE | 2025-12-19 07:20:26.318Z | 85.825° E | 35.186° | 2025-12-19 07:26:26.318Z | 13.116° NNE |
| 9 mins | 2025-12-19 09:03:26.318Z | 232.229° WSW | 2025-12-19 09:07:26.318Z | 281.261° WNW | 25.386° | 2025-12-19 09:12:26.318Z | 334.483° NNW |
| 8 mins | 2025-12-19 18:26:26.318Z | 43.106° NE | 2025-12-19 18:29:26.318Z | 76.065° E | 20.357° | 2025-12-19 18:34:26.318Z | 125.936° SE |
| 11 mins | 2025-12-19 20:11:26.318Z | 350.102° N | 2025-12-19 20:16:26.318Z | 281.643° WNW | 40.708° | 2025-12-19 20:22:26.318Z | 199.773° 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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