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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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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-62
1 62792U 25016H 26092.24595520 .00000030 00000-0 27899-4 0 9993
2 62792 88.9674 91.6476 0017159 30.7792 329.4362 13.51005344 62153Epoch: 2026-04-02T05:54Z
TLE epoch observation values (Epoch: 2026-04-02T05:54:10.529Z)
Latitude
0.00002°
Longitude
172.50654°
Altitude
1,060.516 km
Speed
7.327 km/s
True Right ascension
06h 06m 35s
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
21:30:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.386 km
Perigee altitude
1,052.84 km
Semi-major axis
7,443.75 km
Eccentricity
0.00172
Inclination
88.9674°
RAAN
91.6476°
Arg. of periapsis
30.7792°
True anomaly
329.33603°
Mean anomaly
329.4362°
Eccentric anomaly
329.38613°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.000027899
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-02 23:47:05.959Z | 154.402° SSE | 2026-04-02 23:52:05.959Z | 97.615° ESE | 37.697° | 2026-04-02 23:58:05.959Z | 11.508° NNE |
| 8 mins | 2026-04-03 01:36:05.959Z | 241.335° WSW | 2026-04-03 01:39:05.959Z | 276.199° WNW | 22.372° | 2026-04-03 01:44:05.959Z | 330.048° NNW |
| 8 mins | 2026-04-03 10:58:05.959Z | 38.445° NE | 2026-04-03 11:02:05.959Z | 85.864° E | 22.798° | 2026-04-03 11:06:05.959Z | 127.76° SE |
| 10 mins | 2026-04-03 12:44:05.959Z | 343.872° N | 2026-04-03 12:48:05.959Z | 288.387° WNW | 37.816° | 2026-04-03 12:54:05.959Z | 205.623° SW |
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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