GUANGCHUAN 01, 62111
Orbit data source: Space-Track
GUANGCHUAN 01, 62111 is a payload satellite owned by Hongqing Keji (CN) in LEO that was launched on Wed, 27 Nov 2024 UTC via a ZHUQUE-2E launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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62111 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST?
Mission
Operational Commercial Communications
Bus & Motor
HQ, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
4.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26227.53874920 .00001093 00000-0 73937-4 0 9995
2 62111 49.9440 233.1196 0006855 183.4997 176.5907 15.14965825 95187Epoch: 2026-08-15T12:55Z
TLE epoch observation values (Epoch: 2026-08-15T12:55:47.930Z)
Latitude
-0.00002°
Longitude
75.22169°
Altitude
526.349 km
Speed
7.599 km/s
True Right ascension
15h 32m 28s
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
12:40:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.59 km
Perigee altitude
517.13 km
Semi-major axis
6,899.997 km
Eccentricity
0.00069
Inclination
49.944°
RAAN
233.1196°
Arg. of periapsis
183.4997°
True anomaly
176.59537°
Mean anomaly
176.5907°
Eccentric anomaly
176.59303°
Mean motion
3.78678 °/min
Orbital period
95.07 mins
BSTAR
0.000073937
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Other satellites on launch #221 in the year 2024 (2024-11-27 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.GUANGCHUAN 01 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-16 03:21:44.961Z | 223.625° SW | 2026-08-16 03:24:44.961Z | 166.005° S | 42.402° | 2026-08-16 03:28:44.961Z | 60.404° ENE |
| 5 mins | 2026-08-16 05:02:44.961Z | 299.417° NW | 2026-08-16 05:04:44.961Z | 349.636° N | 25.504° | 2026-08-16 05:07:44.961Z | 40.915° NE |
| 4 mins | 2026-08-16 06:42:44.961Z | 327.198° NNW | 2026-08-16 06:44:44.961Z | 4.431° NNE | 17.934° | 2026-08-16 06:46:44.961Z | 39.417° NE |
| 5 mins | 2026-08-16 08:22:44.961Z | 333.52° NNW | 2026-08-16 08:24:44.961Z | 23.275° NE | 27.499° | 2026-08-16 08:27:44.961Z | 81.822° E |
| 6 mins | 2026-08-16 10:01:44.961Z | 290.112° WNW | 2026-08-16 10:03:44.961Z | 241.591° WSW | 38.911° | 2026-08-16 10:07:44.961Z | 141.259° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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