QIANFAN-44, 62245
Orbit data source: Space-Track
QIANFAN-44, 62245 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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62245 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-44
1 62245U 24232J 26096.91455484 .00000169 00000-0 24287-3 0 9997
2 62245 89.0110 29.4723 0011957 215.0051 145.0315 13.51009398114884Epoch: 2026-04-06T21:56Z
TLE epoch observation values (Epoch: 2026-04-06T21:56:57.538Z)
Latitude
-0.00003°
Longitude
-134.96623°
Altitude
1,078.802 km
Speed
7.309 km/s
True Right ascension
01h 57m 53s
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
14:06:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.498 km
Perigee altitude
1,056.698 km
Semi-major axis
7,443.735 km
Eccentricity
0.0012
Inclination
89.011°
RAAN
29.4723°
Arg. of periapsis
215.0051°
True anomaly
145.10993°
Mean anomaly
145.0315°
Eccentric anomaly
145.07073°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00024287
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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-44 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 | 2026-04-07 09:13:23.014Z | 328.016° NNW | 2026-04-07 09:17:23.014Z | 288.972° WNW | 19.023° | 2026-04-07 09:21:23.014Z | 247.462° WSW |
| 11 mins | 2026-04-07 19:23:23.014Z | 156.499° SSE | 2026-04-07 19:28:23.014Z | 94.776° ESE | 39.466° | 2026-04-07 19:34:23.014Z | 9.7° NNE |
| 8 mins | 2026-04-07 21:12:23.014Z | 244.364° WSW | 2026-04-07 21:15:23.014Z | 278.253° WNW | 21.425° | 2026-04-07 21:20:23.014Z | 329.638° NNW |
| 8 mins | 2026-04-08 06:34:23.014Z | 37.776° NE | 2026-04-08 06:38:23.014Z | 87.143° E | 23.949° | 2026-04-08 06:42:23.014Z | 130.136° SE |
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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