QIANFAN-58, 62788
Orbit data source: Space-Track
QIANFAN-58, 62788 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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62788 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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-58
1 62788U 25016D 25352.57338878 .00000146 00000-0 20709-3 0 9993
2 62788 88.9758 102.4278 0012578 331.2572 28.7884 13.50980026 48034Epoch: 2025-12-18T13:45Z
TLE epoch observation values (Epoch: 2025-12-18T13:45:40.790Z)
Latitude
-0.0001°
Longitude
168.58089°
Altitude
1,063.4 km
Speed
7.324 km/s
True Right ascension
06h 49m 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
20:59:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.069 km
Perigee altitude
1,056.343 km
Semi-major axis
7,443.843 km
Eccentricity
0.00126
Inclination
88.9758°
RAAN
102.4278°
Arg. of periapsis
331.2572°
True anomaly
28.85791°
Mean anomaly
28.7884°
Eccentric anomaly
28.82314°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00020709
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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-58 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-19 07:38:10.065Z | 165.861° S | 2025-12-19 07:44:10.065Z | 77.368° E | 42.911° | 2025-12-19 07:50:10.065Z | 4.886° NNE |
| 7 mins | 2025-12-19 09:28:10.065Z | 252.021° W | 2025-12-19 09:31:10.065Z | 283.39° WNW | 17.557° | 2025-12-19 09:35:10.065Z | 322.664° NNW |
| 10 mins | 2025-12-19 18:49:10.065Z | 28.965° NE | 2025-12-19 18:53:10.065Z | 77.763° E | 28.573° | 2025-12-19 18:59:10.065Z | 144.231° SSE |
| 10 mins | 2025-12-19 20:35:10.065Z | 339.987° N | 2025-12-19 20:40:10.065Z | 275.712° WNW | 32.206° | 2025-12-19 20:45:10.065Z | 217.492° 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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