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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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, 5.0 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 26257.60688507 .00000036 00000-0 37082-4 0 9990
2 62788 88.9644 74.3218 0011988 265.9161 94.0620 13.51019893 84490Epoch: 2026-09-14T14:33Z
TLE epoch observation values (Epoch: 2026-09-14T14:33:54.870Z)
Latitude
0.00001°
Longitude
-137.74159°
Altitude
1,072.105 km
Speed
7.316 km/s
True Right ascension
04h 57m 17s
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
14:59:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.483 km
Perigee altitude
1,056.636 km
Semi-major axis
7,443.697 km
Eccentricity
0.0012
Inclination
88.9644°
RAAN
74.3218°
Arg. of periapsis
265.9161°
True anomaly
94.19901°
Mean anomaly
94.062°
Eccentric anomaly
94.13051°
Mean motion
3.37956 °/min
Orbital period
106.52 mins
BSTAR
0.000037082
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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 | 2026-09-15 00:02:24.724Z | 3.917° NNE | 2026-09-15 00:08:24.724Z | 59.638° ENE | 75.585° | 2026-09-15 00:14:24.724Z | 175.948° S |
| 5 mins | 2026-09-15 01:52:24.724Z | 308.547° NW | 2026-09-15 01:54:24.724Z | 288.061° WNW | 16.585° | 2026-09-15 01:57:24.724Z | 258.625° W |
| 11 mins | 2026-09-15 12:00:24.724Z | 163.987° S | 2026-09-15 12:05:24.724Z | 93.131° ESE | 67.621° | 2026-09-15 12:11:24.724Z | 5.567° NNE |
| 7 mins | 2026-09-15 13:49:24.724Z | 249.564° W | 2026-09-15 13:52:24.724Z | 280.333° WNW | 18.962° | 2026-09-15 13:56:24.724Z | 320.733° NNW |
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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