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, 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-70
1 62800U 25016R 26141.91315617 .00000109 00000-0 15039-3 0 9998
2 62800 88.9726 86.4891 0013336 228.2967 131.7044 13.51013046 68868Epoch: 2026-05-21T21:54Z
TLE epoch observation values (Epoch: 2026-05-21T21:54:56.693Z)
Latitude
0°
Longitude
-121.79866°
Altitude
1,078.102 km
Speed
7.31 km/s
True Right ascension
05h 45m 57s
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
15:19:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.512 km
Perigee altitude
1,055.658 km
Semi-major axis
7,443.722 km
Eccentricity
0.00133
Inclination
88.9726°
RAAN
86.4891°
Arg. of periapsis
228.2967°
True anomaly
131.81837°
Mean anomaly
131.7044°
Eccentric anomaly
131.7614°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00015039
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-22 07:24:30.799Z | 28.397° NE | 2026-05-22 07:29:30.799Z | 80.97° E | 23.06° | 2026-05-22 07:34:30.799Z | 132.256° SE |
| 11 mins | 2026-05-22 09:11:30.799Z | 345.156° N | 2026-05-22 09:16:30.799Z | 268.952° W | 37.634° | 2026-05-22 09:22:30.799Z | 204.19° SW |
| 8 mins | 2026-05-22 19:23:30.799Z | 114.759° SE | 2026-05-22 19:27:30.799Z | 71.507° E | 20.785° | 2026-05-22 19:31:30.799Z | 31.225° NE |
| 11 mins | 2026-05-22 21:08:30.799Z | 198.465° SSW | 2026-05-22 21:13:30.799Z | 283.426° WNW | 40.313° | 2026-05-22 21:19:30.799Z | 350.767° N |
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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