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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-58
1 62788U 25016D 26307.59859947 .00000095 00000-0 12790-3 0 9995
2 62788 88.9708 69.1088 0015505 120.1217 240.1473 13.51031883 91245Epoch: 2026-11-03T14:21Z
TLE epoch observation values (Epoch: 2026-11-03T14:21:58.994Z)
Latitude
-0.00003°
Longitude
170.75403°
Altitude
1,077.18 km
Speed
7.311 km/s
True Right ascension
04h 36m 26s
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
19:21:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.057 km
Perigee altitude
1,053.974 km
Semi-major axis
7,443.653 km
Eccentricity
0.00155
Inclination
88.9708°
RAAN
69.1088°
Arg. of periapsis
120.1217°
True anomaly
239.99335°
Mean anomaly
240.1473°
Eccentric anomaly
240.07031°
Mean motion
3.37959 °/min
Orbital period
106.52 mins
BSTAR
0.0001279
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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 | 2026-11-04 08:14:38.550Z | 159.636° S | 2026-11-04 08:20:38.550Z | 72.276° E | 58.293° | 2026-11-04 08:26:38.550Z | 7.406° NNE |
| 8 mins | 2026-11-04 10:03:38.550Z | 242.206° WSW | 2026-11-04 10:07:38.550Z | 285.996° WNW | 21.676° | 2026-11-04 10:11:38.550Z | 326.28° NNW |
| 9 mins | 2026-11-04 19:25:38.550Z | 34.008° NE | 2026-11-04 19:29:38.550Z | 82.504° E | 28.014° | 2026-11-04 19:34:38.550Z | 135.951° SSE |
| 10 mins | 2026-11-04 21:11:38.550Z | 342.065° N | 2026-11-04 21:16:38.550Z | 267.875° W | 44.679° | 2026-11-04 21:21:38.550Z | 210.841° 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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