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: 12 hours ago
TLE from 12 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26171.40225868 .00003221 00000-0 18789-3 0 9998
2 62111 49.9429 146.4966 0007653 313.9258 46.1060 15.14649947 86672Epoch: 2026-06-20T09:39Z
TLE epoch observation values (Epoch: 2026-06-20T09:39:15.149Z)
Latitude
-0.00007°
Longitude
93.06603°
Altitude
518.928 km
Speed
7.607 km/s
True Right ascension
09h 45m 59s
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
08:43:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.101 km
Perigee altitude
517.538 km
Semi-major axis
6,900.957 km
Eccentricity
0.00077
Inclination
49.9429°
RAAN
146.4966°
Arg. of periapsis
313.9258°
True anomaly
46.16924°
Mean anomaly
46.106°
Eccentric anomaly
46.13762°
Mean motion
3.78599 °/min
Orbital period
95.09 mins
BSTAR
0.00018789
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 00:04:02.401Z | 162.055° S | 2026-06-21 00:06:02.401Z | 127.533° SE | 15.75° | 2026-06-21 00:08:02.401Z | 95.35° ESE |
| 6 mins | 2026-06-21 01:42:02.401Z | 242.723° WSW | 2026-06-21 01:45:02.401Z | 19.77° NNE | 42.911° | 2026-06-21 01:48:02.401Z | 52.82° ENE |
| 4 mins | 2026-06-21 03:23:02.401Z | 315.735° NNW | 2026-06-21 03:24:02.401Z | 337.407° NNW | 21.674° | 2026-06-21 03:27:02.401Z | 35.009° NE |
| 4 mins | 2026-06-21 05:03:02.401Z | 335.724° NNW | 2026-06-21 05:05:02.401Z | 15.29° NNE | 18.592° | 2026-06-21 05:07:02.401Z | 48.918° ENE |
| 6 mins | 2026-06-21 06:42:02.401Z | 321.438° NNW | 2026-06-21 06:45:02.401Z | 45.029° ENE | 33.364° | 2026-06-21 06:48:02.401Z | 97.058° ESE |
| 5 mins | 2026-06-21 08:22:02.401Z | 269.578° W | 2026-06-21 08:24:02.401Z | 214.79° SW | 28.908° | 2026-06-21 08:27:02.401Z | 160.246° 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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