QIANFAN-59, 62789
Orbit data source: Space-Track
QIANFAN-59, 62789 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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62789 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, 1.5 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-59
1 62789U 25016E 25306.45592035 .00000060 00000-0 73355-4 0 9998
2 62789 88.9745 107.2641 0015931 102.6087 257.6847 13.50976364 41805Epoch: 2025-11-02T10:56Z
TLE epoch observation values (Epoch: 2025-11-02T10:56:31.518Z)
Latitude
0.00002°
Longitude
-98.83862°
Altitude
1,074.171 km
Speed
7.314 km/s
True Right ascension
07h 09m 03s
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
14:39:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.578 km
Perigee altitude
1,053.861 km
Semi-major axis
7,443.857 km
Eccentricity
0.00159
Inclination
88.9745°
RAAN
107.2641°
Arg. of periapsis
102.6087°
True anomaly
257.50642°
Mean anomaly
257.6847°
Eccentric anomaly
257.59555°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000073355
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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-59 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 21:20:49.343Z | 48.851° ENE | 2025-11-03 21:23:49.343Z | 76.6° E | 12.541° | 2025-11-03 21:25:49.343Z | 95.151° ESE |
| 11 mins | 2025-11-03 23:05:49.343Z | 1.3° NNE | 2025-11-03 23:10:49.343Z | 17.304° NNE | 44.949° | 2025-11-03 23:16:49.343Z | 182.262° SSW |
| 4 mins | 2025-11-04 00:54:49.343Z | 305.736° NW | 2025-11-04 00:56:49.343Z | 286.334° WNW | 13.172° | 2025-11-04 00:58:49.343Z | 267.547° W |
| 11 mins | 2025-11-04 11:02:49.343Z | 170.908° S | 2025-11-04 11:07:49.343Z | 103.286° ESE | 44.409° | 2025-11-04 11:13:49.343Z | 2.251° NNE |
| 6 mins | 2025-11-04 12:52:49.343Z | 260.561° W | 2025-11-04 12:54:49.343Z | 280.36° WNW | 15.008° | 2025-11-04 12:58:49.343Z | 318.665° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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