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 25325.07920955 .00000038 00000-0 39798-4 0 9993
2 62790 88.9743 105.3150 0016817 50.8658 309.3984 13.50976927 44301Epoch: 2025-11-21T01:54Z
TLE epoch observation values (Epoch: 2025-11-21T01:54:03.705Z)
Latitude
-0.00009°
Longitude
16.47217°
Altitude
1,063.682 km
Speed
7.324 km/s
True Right ascension
07h 01m 15s
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
10:37:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.236 km
Perigee altitude
1,053.199 km
Semi-major axis
7,443.855 km
Eccentricity
0.00168
Inclination
88.9743°
RAAN
105.315°
Arg. of periapsis
50.8658°
True anomaly
309.24929°
Mean anomaly
309.3984°
Eccentric anomaly
309.32386°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000039798
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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 | 2025-11-21 20:17:43.196Z | 39.923° NE | 2025-11-21 20:21:43.196Z | 79.968° E | 17.154° | 2025-11-21 20:25:43.196Z | 117.698° SE |
| 11 mins | 2025-11-21 22:03:43.196Z | 353.65° N | 2025-11-21 22:08:43.196Z | 263.859° W | 43.211° | 2025-11-21 22:14:43.196Z | 192.856° SSW |
| 5 mins | 2025-11-22 08:17:43.196Z | 93.657° ESE | 2025-11-22 08:19:43.196Z | 73.592° E | 14.997° | 2025-11-22 08:22:43.196Z | 44.136° NE |
| 11 mins | 2025-11-22 10:00:43.196Z | 183.524° SSW | 2025-11-22 10:05:43.196Z | 289.605° WNW | 44.49° | 2025-11-22 10:11:43.196Z | 356.621° N |
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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