QIANFAN-70, 62800
Orbit data source: Space-Track
QIANFAN-70, 62800 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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62800 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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-70
1 62800U 25016R 26035.78085932 .00000106 00000-0 14534-3 0 9995
2 62800 88.9733 97.5255 0016116 172.2930 187.8471 13.50994140 54537Epoch: 2026-02-04T18:44Z
TLE epoch observation values (Epoch: 2026-02-04T18:44:26.245Z)
Latitude
-0.0001°
Longitude
41.47362°
Altitude
1,083.448 km
Speed
7.305 km/s
True Right ascension
06h 30m 06s
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
03:17:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.651 km
Perigee altitude
1,053.658 km
Semi-major axis
7,443.791 km
Eccentricity
0.00161
Inclination
88.9733°
RAAN
97.5255°
Arg. of periapsis
172.293°
True anomaly
187.82194°
Mean anomaly
187.8471°
Eccentric anomaly
187.83451°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.00014534
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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-70 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 03:43:48.544Z | 149.041° SSE | 2026-02-05 03:49:48.544Z | 79.81° E | 34.39° | 2026-02-05 03:55:48.544Z | 13.145° NNE |
| 10 mins | 2026-02-05 05:31:48.544Z | 225.585° WSW | 2026-02-05 05:36:48.544Z | 285.214° WNW | 26.355° | 2026-02-05 05:41:48.544Z | 336.537° NNW |
| 7 mins | 2026-02-05 14:55:48.544Z | 46.341° ENE | 2026-02-05 14:58:48.544Z | 79.78° E | 19.17° | 2026-02-05 15:02:48.544Z | 120.243° SE |
| 11 mins | 2026-02-05 16:40:48.544Z | 350.458° N | 2026-02-05 16:45:48.544Z | 268.656° W | 41.363° | 2026-02-05 16:51:48.544Z | 197.389° 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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