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: 15 hours ago
TLE from 15 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 25347.00887679 .00007902 00000-0 42288-3 0 9993
2 62111 49.9448 349.4832 0007176 273.4606 86.5525 15.15832311 57950Epoch: 2025-12-13T00:12Z
TLE epoch observation values (Epoch: 2025-12-13T00:12:46.954Z)
Latitude
0.00003°
Longitude
-95.65472°
Altitude
518.705 km
Speed
7.606 km/s
True Right ascension
23h 17m 55s
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
13:39:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.181 km
Perigee altitude
514.282 km
Semi-major axis
6,897.368 km
Eccentricity
0.00072
Inclination
49.9448°
RAAN
349.4832°
Arg. of periapsis
273.4606°
True anomaly
86.63459°
Mean anomaly
86.5525°
Eccentric anomaly
86.59354°
Mean motion
3.78894 °/min
Orbital period
95.01 mins
BSTAR
0.00042288
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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 | 2025-12-14 03:19:20.356Z | 234.123° WSW | 2025-12-14 03:21:20.356Z | 224.313° SW | 44.817° | 2025-12-14 03:25:20.356Z | 56.173° ENE |
| 5 mins | 2025-12-14 04:59:20.356Z | 305.787° NW | 2025-12-14 05:01:20.356Z | 351.834° N | 23.06° | 2025-12-14 05:04:20.356Z | 40.995° NE |
| 4 mins | 2025-12-14 06:39:20.356Z | 330.275° NNW | 2025-12-14 06:41:20.356Z | 7.953° NNE | 18.271° | 2025-12-14 06:43:20.356Z | 43.109° NE |
| 5 mins | 2025-12-14 08:19:20.356Z | 333.472° NNW | 2025-12-14 08:21:20.356Z | 32.047° NE | 30.951° | 2025-12-14 08:24:20.356Z | 90.055° ESE |
| 5 mins | 2025-12-14 09:58:20.356Z | 278.554° WNW | 2025-12-14 10:00:20.356Z | 221.102° SW | 33.648° | 2025-12-14 10:03:20.356Z | 154.485° 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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