QIANFAN-62, 62792
Orbit data source: Space-Track
QIANFAN-62, 62792 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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62792 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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-62
1 62792U 25016H 25354.14929985 .00000144 00000-0 20439-3 0 9996
2 62792 88.9776 102.3428 0014695 325.6006 34.4192 13.50978867 48234Epoch: 2025-12-20T03:34Z
TLE epoch observation values (Epoch: 2025-12-20T03:34:59.507Z)
Latitude
-0.00005°
Longitude
-40.38539°
Altitude
1,062.589 km
Speed
7.325 km/s
True Right ascension
06h 49m 22s
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
09:53:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.649 km
Perigee altitude
1,054.772 km
Semi-major axis
7,443.847 km
Eccentricity
0.00147
Inclination
88.9776°
RAAN
102.3428°
Arg. of periapsis
325.6006°
True anomaly
34.51453°
Mean anomaly
34.4192°
Eccentric anomaly
34.46685°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00020439
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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-62 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-20 18:25:03.262Z | 33.626° NE | 2025-12-20 18:29:03.262Z | 75.221° E | 21.596° | 2025-12-20 18:34:03.262Z | 127.27° SE |
| 11 mins | 2025-12-20 20:11:03.262Z | 348.672° N | 2025-12-20 20:16:03.262Z | 282.839° WNW | 39.449° | 2025-12-20 20:22:03.262Z | 202.427° SSW |
| 7 mins | 2025-12-21 06:24:03.262Z | 108.705° ESE | 2025-12-21 06:27:03.262Z | 77.118° E | 19.102° | 2025-12-21 06:31:03.262Z | 35.573° NE |
| 11 mins | 2025-12-21 08:08:03.262Z | 193.416° SSW | 2025-12-21 08:13:03.262Z | 264.284° W | 41.761° | 2025-12-21 08:19:03.262Z | 351.374° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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