QIANFAN-45, 62246
Orbit data source: Space-Track
QIANFAN-45, 62246 is a Chinese payload satellite in LEO that was launched on Thu, 05 Dec 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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62246 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-45
1 62246U 24232K 26096.88158315 .00000169 00000-0 24285-3 0 9995
2 62246 89.0113 29.6261 0012639 215.0056 145.0266 13.51013193114805Epoch: 2026-04-06T21:09Z
TLE epoch observation values (Epoch: 2026-04-06T21:09:28.784Z)
Latitude
0.00005°
Longitude
-122.91012°
Altitude
1,079.204 km
Speed
7.309 km/s
True Right ascension
01h 58m 30s
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
14:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.992 km
Perigee altitude
1,056.176 km
Semi-major axis
7,443.721 km
Eccentricity
0.00126
Inclination
89.0113°
RAAN
29.6261°
Arg. of periapsis
215.0056°
True anomaly
145.10951°
Mean anomaly
145.0266°
Eccentric anomaly
145.06807°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00024285
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Other satellites on launch #232 in the year 2024 (2024-12-05 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-45 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 | 2026-04-07 08:25:06.908Z | 346.958° N | 2026-04-07 08:31:06.908Z | 267.629° W | 35.941° | 2026-04-07 08:36:06.908Z | 209.655° SW |
| 8 mins | 2026-04-07 18:38:06.908Z | 116.025° SE | 2026-04-07 18:42:06.908Z | 70.305° E | 22.194° | 2026-04-07 18:46:06.908Z | 29.499° NE |
| 11 mins | 2026-04-07 20:23:06.908Z | 202.167° SSW | 2026-04-07 20:28:06.908Z | 284.271° WNW | 38.764° | 2026-04-07 20:34:06.908Z | 349.468° N |
| 11 mins | 2026-04-08 07:32:06.908Z | 6.015° NNE | 2026-04-08 07:37:06.908Z | 68.573° E | 43.857° | 2026-04-08 07:43:06.908Z | 174.753° S |
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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