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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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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-70
1 62800U 25016R 26257.59858412 .00000053 00000-0 63729-4 0 9993
2 62800 88.9665 74.4580 0013559 257.0645 102.8992 13.51023515 84481Epoch: 2026-09-14T14:21Z
TLE epoch observation values (Epoch: 2026-09-14T14:21:57.667Z)
Latitude
-0.00005°
Longitude
-134.60886°
Altitude
1,073.716 km
Speed
7.314 km/s
True Right ascension
04h 57m 49s
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
14:58:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.639 km
Perigee altitude
1,055.453 km
Semi-major axis
7,443.683 km
Eccentricity
0.00136
Inclination
88.9665°
RAAN
74.458°
Arg. of periapsis
257.0645°
True anomaly
103.0506°
Mean anomaly
102.8992°
Eccentric anomaly
102.9749°
Mean motion
3.37957 °/min
Orbital period
106.52 mins
BSTAR
0.000063729
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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 | 2026-09-14 23:50:51.361Z | 8.826° NNE | 2026-09-14 23:56:51.361Z | 91.692° ESE | 62.499° | 2026-09-15 00:02:51.361Z | 168.035° S |
| 7 mins | 2026-09-15 01:39:51.361Z | 316.936° NNW | 2026-09-15 01:42:51.361Z | 283.776° WNW | 20.867° | 2026-09-15 01:46:51.361Z | 243.931° WSW |
| 11 mins | 2026-09-15 11:48:51.361Z | 153.701° SSE | 2026-09-15 11:53:51.361Z | 76.999° E | 54.314° | 2026-09-15 11:59:51.361Z | 9.071° NNE |
| 8 mins | 2026-09-15 13:36:51.361Z | 239.639° WSW | 2026-09-15 13:40:51.361Z | 285.031° WNW | 23.805° | 2026-09-15 13:44:51.361Z | 326.774° NNW |
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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