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 26035.78900499 .00000121 00000-0 16900-3 0 9990
2 62788 88.9712 97.4360 0014328 178.9491 181.1693 13.50995535 54546Epoch: 2026-02-04T18:56Z
TLE epoch observation values (Epoch: 2026-02-04T18:56:10.031Z)
Latitude
0.00002°
Longitude
38.44365°
Altitude
1,082.221 km
Speed
7.306 km/s
True Right ascension
06h 29m 44s
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
05:00:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.315 km
Perigee altitude
1,054.984 km
Semi-major axis
7,443.786 km
Eccentricity
0.00143
Inclination
88.9712°
RAAN
97.436°
Arg. of periapsis
178.9491°
True anomaly
181.16596°
Mean anomaly
181.1693°
Eccentric anomaly
181.16763°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.000169
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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 | 2026-02-05 03:55:34.632Z | 156.209° SSE | 2026-02-05 04:01:34.632Z | 76.854° E | 38.721° | 2026-02-05 04:07:34.632Z | 9.316° NNE |
| 8 mins | 2026-02-05 05:44:34.632Z | 239.268° WSW | 2026-02-05 05:48:34.632Z | 285.2° WNW | 22.207° | 2026-02-05 05:52:34.632Z | 327.167° NNW |
| 9 mins | 2026-02-05 15:06:34.632Z | 34.848° NE | 2026-02-05 15:10:34.632Z | 80.664° E | 23.212° | 2026-02-05 15:15:34.632Z | 132.572° SE |
| 10 mins | 2026-02-05 16:52:34.632Z | 344.934° N | 2026-02-05 16:57:34.632Z | 269.816° W | 37.274° | 2026-02-05 17:02:34.632Z | 207.748° 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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