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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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 26092.28286157 .00000043 00000-0 48496-4 0 9998
2 62790 88.9661 91.5968 0016859 31.0459 329.1684 13.51010506 62152Epoch: 2026-04-02T06:47Z
TLE epoch observation values (Epoch: 2026-04-02T06:47:19.239Z)
Latitude
-0.00012°
Longitude
159.13306°
Altitude
1,060.719 km
Speed
7.327 km/s
True Right ascension
06h 06m 23s
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
21:31:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.144 km
Perigee altitude
1,053.045 km
Semi-major axis
7,443.731 km
Eccentricity
0.00169
Inclination
88.9661°
RAAN
91.5968°
Arg. of periapsis
31.0459°
True anomaly
329.06921°
Mean anomaly
329.1684°
Eccentric anomaly
329.11882°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.000048496
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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 | 2026-04-02 22:55:39.471Z | 114.723° SE | 2026-04-02 22:59:39.471Z | 74.276° E | 18.958° | 2026-04-02 23:03:39.471Z | 33.762° NE |
| 11 mins | 2026-04-03 00:40:39.471Z | 194.056° SSW | 2026-04-03 00:45:39.471Z | 275.577° WNW | 41.747° | 2026-04-03 00:51:39.471Z | 351.941° N |
| 12 mins | 2026-04-03 11:49:39.471Z | 9.322° NNE | 2026-04-03 11:54:39.471Z | 67.315° ENE | 41.588° | 2026-04-03 12:01:39.471Z | 169.921° S |
| 7 mins | 2026-04-03 13:37:39.471Z | 321.098° NNW | 2026-04-03 13:40:39.471Z | 290.069° WNW | 18.995° | 2026-04-03 13:44:39.471Z | 248.344° W |
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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