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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-58
1 62788U 25016D 26092.22530110 .00000025 00000-0 19225-4 0 9998
2 62788 88.9656 91.5526 0014956 31.8600 328.3452 13.51000126 62167Epoch: 2026-04-02T05:24Z
TLE epoch observation values (Epoch: 2026-04-02T05:24:26.015Z)
Latitude
-0.00007°
Longitude
179.86737°
Altitude
1,062.057 km
Speed
7.326 km/s
True Right ascension
06h 06m 12s
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
23:16:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.765 km
Perigee altitude
1,054.499 km
Semi-major axis
7,443.769 km
Eccentricity
0.0015
Inclination
88.9656°
RAAN
91.5526°
Arg. of periapsis
31.86°
True anomaly
328.25511°
Mean anomaly
328.3452°
Eccentric anomaly
328.30017°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.000019225
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-02 23:18:05.613Z | 133.98° SE | 2026-04-02 23:23:05.613Z | 78.561° E | 27.086° | 2026-04-02 23:28:05.613Z | 22.709° NE |
| 10 mins | 2026-04-03 01:05:05.613Z | 214.719° SW | 2026-04-03 01:09:05.613Z | 267.803° W | 33.159° | 2026-04-03 01:15:05.613Z | 342.873° N |
| 4 mins | 2026-04-03 10:30:05.613Z | 60.334° ENE | 2026-04-03 10:31:05.613Z | 70.139° E | 13.847° | 2026-04-03 10:34:05.613Z | 98.95° ESE |
| 11 mins | 2026-04-03 12:14:05.613Z | 359.266° N | 2026-04-03 12:19:05.613Z | 226.675° WSW | 44.797° | 2026-04-03 12:25:05.613Z | 185.139° SSW |
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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