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 26305.02813748 -.01956920 00000-0 -34490+1 0 9995
2 62245 89.0152 8.6773 0015107 332.1604 27.8735 13.47372810142982Epoch: 2026-11-01T00:40Z
TLE epoch observation values (Epoch: 2026-11-01T00:40:31.078Z)
Latitude
-0.00003°
Longitude
-41.77759°
Altitude
1,074.928 km
Speed
7.319 km/s
True Right ascension
00h 34m 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
06:21:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,090.262 km
Perigee altitude
1,067.731 km
Semi-major axis
7,457.133 km
Eccentricity
0.00151
Inclination
89.0152°
RAAN
8.6773°
Arg. of periapsis
332.1604°
True anomaly
27.95457°
Mean anomaly
27.8735°
Eccentric anomaly
27.91402°
Mean motion
3.37043 °/min
Orbital period
106.81 mins
BSTAR
-3.449
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-01 15:32:55.294Z | 25.568° NE | 2026-11-01 15:37:55.294Z | 76.016° E | 27.757° | 2026-11-01 15:42:55.294Z | 131.798° SE |
| 11 mins | 2026-11-01 17:20:55.294Z | 342.449° N | 2026-11-01 17:25:55.294Z | 266.1° W | 47.173° | 2026-11-01 17:31:55.294Z | 206.601° SW |
| 9 mins | 2026-11-02 03:35:55.294Z | 119.192° SE | 2026-11-02 03:39:55.294Z | 73.219° E | 26.157° | 2026-11-02 03:44:55.294Z | 24.057° NE |
| 11 mins | 2026-11-02 05:21:55.294Z | 205.802° SW | 2026-11-02 05:26:55.294Z | 286.206° WNW | 49.934° | 2026-11-02 05:32:55.294Z | 348.418° 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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