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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 25340.81205943 .00007489 00000-0 40263-3 0 9994
2 62111 49.9460 19.7049 0007407 248.9528 111.0631 15.15740837 57018Epoch: 2025-12-06T19:29Z
TLE epoch observation values (Epoch: 2025-12-06T19:29:21.934Z)
Latitude
-0.00005°
Longitude
11.52904°
Altitude
521.115 km
Speed
7.603 km/s
True Right ascension
01h 18m 49s
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
04:25:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.617 km
Perigee altitude
514.399 km
Semi-major axis
6,897.645 km
Eccentricity
0.00074
Inclination
49.946°
RAAN
19.7049°
Arg. of periapsis
248.9528°
True anomaly
111.14228°
Mean anomaly
111.0631°
Eccentric anomaly
111.10269°
Mean motion
3.78871 °/min
Orbital period
95.02 mins
BSTAR
0.00040263
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 06:47:52.742Z | 264.616° W | 2025-12-07 06:50:52.742Z | 329.312° NNW | 34.274° | 2025-12-07 06:53:52.742Z | 41.395° NE |
| 5 mins | 2025-12-07 10:08:52.742Z | 330.861° NNW | 2025-12-07 10:10:52.742Z | 9.809° NNE | 21.692° | 2025-12-07 10:13:52.742Z | 64.998° ENE |
| 6 mins | 2025-12-07 11:47:52.742Z | 308.57° NW | 2025-12-07 11:50:52.742Z | 62.055° ENE | 43.773° | 2025-12-07 11:53:52.742Z | 117.851° SE |
| 5 mins | 2025-12-08 04:53:52.742Z | 195.491° SSW | 2025-12-08 04:55:52.742Z | 147.702° SSE | 31.567° | 2025-12-08 04:58:52.742Z | 75.506° E |
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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