GUANGCHUAN 01, 62111
Orbit data source: Space-Track
GUANGCHUAN 01, 62111 is a Chinese payload satellite 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
LTZH
Mission
Operational Commercial Communications
Bus & Motor
GUANGCHUAN, Unknown motor
Mass
~250 kg wet, ~250 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: 7 hours ago
TLE from 7 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26306.11715686 .00001538 00000-0 98406-4 0 9992
2 62111 49.9431 210.6046 0007039 136.0645 224.0866 15.14586820107091Epoch: 2026-11-02T02:48Z
TLE epoch observation values (Epoch: 2026-11-02T02:48:42.352Z)
Latitude
-0.00005°
Longitude
127.02931°
Altitude
526.269 km
Speed
7.599 km/s
True Right ascension
14h 02m 25s
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
05:13:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.869 km
Perigee altitude
518.154 km
Semi-major axis
6,901.148 km
Eccentricity
0.0007
Inclination
49.9431°
RAAN
210.6046°
Arg. of periapsis
136.0645°
True anomaly
224.03052°
Mean anomaly
224.0866°
Eccentric anomaly
224.05855°
Mean motion
3.78583 °/min
Orbital period
95.09 mins
BSTAR
0.000098406
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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 | 2026-11-02 20:23:49.855Z | 215.846° SW | 2026-11-02 20:27:49.855Z | 120.329° SE | 49.885° | 2026-11-02 20:30:49.855Z | 66.069° ENE |
| 5 mins | 2026-11-02 22:04:49.855Z | 287.347° WNW | 2026-11-02 22:06:49.855Z | 336.364° NNW | 32.939° | 2026-11-02 22:09:49.855Z | 38.445° NE |
| 4 mins | 2026-11-02 23:45:49.855Z | 335.346° NNW | 2026-11-02 23:46:49.855Z | 354.792° N | 18.9° | 2026-11-02 23:49:49.855Z | 44.254° NE |
| 5 mins | 2026-11-03 01:24:49.855Z | 329.184° NNW | 2026-11-03 01:26:49.855Z | 8.931° NNE | 27.002° | 2026-11-03 01:29:49.855Z | 71.387° E |
| 6 mins | 2026-11-03 03:03:49.855Z | 299.945° NW | 2026-11-03 03:06:49.855Z | 197.136° SSW | 74.205° | 2026-11-03 03:09:49.855Z | 132.792° SE |
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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