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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-60
1 62790U 25016F 25258.88226735 .00000047 00000-0 52937-4 0 9992
2 62790 88.9752 112.1765 0013755 235.1113 124.8747 13.52522877 35367Epoch: 2025-09-15T21:10Z
TLE epoch observation values (Epoch: 2025-09-15T21:10:27.899Z)
Latitude
0.00003°
Longitude
159.47971°
Altitude
1,071.809 km
Speed
7.313 km/s
True Right ascension
07h 28m 42s
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
02:37:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,070.271 km
Perigee altitude
1,049.808 km
Semi-major axis
7,438.177 km
Eccentricity
0.00138
Inclination
88.9752°
RAAN
112.1765°
Arg. of periapsis
235.1113°
True anomaly
125.00389°
Mean anomaly
124.8747°
Eccentric anomaly
124.93931°
Mean motion
3.38332 °/min
Orbital period
106.4 mins
BSTAR
0.000052937
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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 | 2025-09-16 13:17:24.186Z | 116.353° SE | 2025-09-16 13:21:24.186Z | 78.819° E | 18.415° | 2025-09-16 13:25:24.186Z | 37.362° NE |
| 11 mins | 2025-09-16 15:02:24.186Z | 191.512° SSW | 2025-09-16 15:07:24.186Z | 261.72° W | 42.44° | 2025-09-16 15:13:24.186Z | 352.203° N |
| 11 mins | 2025-09-17 02:11:24.186Z | 11.707° NNE | 2025-09-17 02:16:24.186Z | 85.484° E | 41.022° | 2025-09-17 02:22:24.186Z | 166.691° S |
| 7 mins | 2025-09-17 03:59:24.186Z | 317.675° NNW | 2025-09-17 04:02:24.186Z | 284.035° WNW | 19.932° | 2025-09-17 04:06:24.186Z | 243.31° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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