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 26037.64059552 .00000101 00000-0 13819-3 0 9996
2 62788 88.9710 97.2437 0014499 173.7828 186.3506 13.50995891 54795Epoch: 2026-02-06T15:22Z
TLE epoch observation values (Epoch: 2026-02-06T15:22:27.452Z)
Latitude
-0.00002°
Longitude
89.85375°
Altitude
1,082.283 km
Speed
7.306 km/s
True Right ascension
06h 28m 58s
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
01:25:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.441 km
Perigee altitude
1,054.855 km
Semi-major axis
7,443.785 km
Eccentricity
0.00145
Inclination
88.971°
RAAN
97.2437°
Arg. of periapsis
173.7828°
True anomaly
186.33226°
Mean anomaly
186.3506°
Eccentric anomaly
186.34142°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.00013819
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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 | 2026-02-07 03:55:14.035Z | 161.447° S | 2026-02-07 04:01:14.035Z | 70.979° E | 41.232° | 2026-02-07 04:07:14.035Z | 6.566° NNE |
| 8 mins | 2026-02-07 05:44:14.035Z | 243.277° WSW | 2026-02-07 05:48:14.035Z | 285.799° WNW | 19.517° | 2026-02-07 05:52:14.035Z | 325.486° NNW |
| 9 mins | 2026-02-07 15:06:14.035Z | 32.774° NE | 2026-02-07 15:10:14.035Z | 82.041° E | 26.136° | 2026-02-07 15:15:14.035Z | 137.22° SSE |
| 10 mins | 2026-02-07 16:52:14.035Z | 341.111° N | 2026-02-07 16:57:14.035Z | 269.378° W | 34.061° | 2026-02-07 17:02:14.035Z | 212.678° 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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