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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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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-17
1 60395U 24140S 26114.52965545 .00000038 00000-0 40060-4 0 9994
2 60395 88.9694 285.6791 0015210 175.2299 184.9000 13.51008593 86068Epoch: 2026-04-24T12:42Z
TLE epoch observation values (Epoch: 2026-04-24T12:42:42.230Z)
Latitude
-0.00003°
Longitude
-117.55792°
Altitude
1,082.791 km
Speed
7.305 km/s
True Right ascension
19h 02m 42s
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
00:38:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.923 km
Perigee altitude
1,054.279 km
Semi-major axis
7,443.738 km
Eccentricity
0.00152
Inclination
88.9694°
RAAN
285.6791°
Arg. of periapsis
175.2299°
True anomaly
184.88514°
Mean anomaly
184.9°
Eccentric anomaly
184.89257°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00004006
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-24 22:12:37.370Z | 35.199° NE | 2026-04-24 22:16:37.370Z | 73.321° E | 17.399° | 2026-04-24 22:20:37.370Z | 113.932° SE |
| 11 mins | 2026-04-24 23:58:37.370Z | 354.088° N | 2026-04-25 00:03:37.370Z | 298.503° NW | 42.545° | 2026-04-25 00:09:37.370Z | 194.552° SSW |
| 6 mins | 2026-04-25 10:12:37.370Z | 98.45° ESE | 2026-04-25 10:15:37.370Z | 68.484° E | 15.646° | 2026-04-25 10:18:37.370Z | 40.108° NE |
| 12 mins | 2026-04-25 11:55:37.370Z | 183.923° SSW | 2026-04-25 12:00:37.370Z | 234.337° WSW | 44.124° | 2026-04-25 12:07:37.370Z | 356.615° 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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