QIANFAN-17, 60395
Orbit data source: Space-Track
QIANFAN-17, 60395 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 2024 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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60395 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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 QIANFAN-17
1 60395U 24140S 25312.81222588 .00000048 00000-0 55966-4 0 9990
2 60395 88.9741 302.9481 0013459 309.4479 50.5481 13.50971656 63552Epoch: 2025-11-08T19:29Z
TLE epoch observation values (Epoch: 2025-11-08T19:29:36.316Z)
Latitude
0.00006°
Longitude
-37.68968°
Altitude
1,065.277 km
Speed
7.322 km/s
True Right ascension
20h 11m 47s
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
04:58:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.756 km
Perigee altitude
1,055.718 km
Semi-major axis
7,443.874 km
Eccentricity
0.00135
Inclination
88.9741°
RAAN
302.9481°
Arg. of periapsis
309.4479°
True anomaly
50.66732°
Mean anomaly
50.5481°
Eccentric anomaly
50.6077°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000055966
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Other satellites on launch #140 in the year 2024 (2024-08-06 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-17 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-10 11:11:57.774Z | 13.251° NNE | 2025-11-10 11:17:57.774Z | 102.406° ESE | 38.289° | 2025-11-10 11:22:57.774Z | 160.337° S |
| 8 mins | 2025-11-10 12:59:57.774Z | 324.667° NNW | 2025-11-10 13:03:57.774Z | 278.535° WNW | 22.454° | 2025-11-10 13:07:57.774Z | 237.575° WSW |
| 10 mins | 2025-11-10 23:09:57.774Z | 146.126° SSE | 2025-11-10 23:14:57.774Z | 70.7° E | 35.554° | 2025-11-10 23:19:57.774Z | 14.057° NNE |
| 9 mins | 2025-11-11 00:56:57.774Z | 229.96° WSW | 2025-11-11 01:00:57.774Z | 275.078° WNW | 24.896° | 2025-11-11 01:05:57.774Z | 331.513° 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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