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: 9 hours ago
TLE from 9 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26035.85514170 .00006083 00000-0 32315-3 0 9993
2 62111 49.9428 86.7243 0006369 129.5537 230.5978 15.16507752 66123Epoch: 2026-02-04T20:31Z
TLE epoch observation values (Epoch: 2026-02-04T20:31:24.242Z)
Latitude
-0.00003°
Longitude
3.85753°
Altitude
519.74 km
Speed
7.603 km/s
True Right ascension
05h 46m 53s
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
07:30:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.575 km
Perigee altitude
512.792 km
Semi-major axis
6,895.321 km
Eccentricity
0.00064
Inclination
49.9428°
RAAN
86.7243°
Arg. of periapsis
129.5537°
True anomaly
230.54143°
Mean anomaly
230.5978°
Eccentric anomaly
230.56961°
Mean motion
3.79063 °/min
Orbital period
94.97 mins
BSTAR
0.00032315
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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 | 2026-02-05 06:11:37.816Z | 220.176° SW | 2026-02-05 06:14:37.816Z | 158.127° S | 40.952° | 2026-02-05 06:18:37.816Z | 61.749° ENE |
| 4 mins | 2026-02-05 07:52:37.816Z | 300.293° NW | 2026-02-05 07:54:37.816Z | 354.364° N | 25.729° | 2026-02-05 07:56:37.816Z | 33.384° NE |
| 4 mins | 2026-02-05 09:32:37.816Z | 330.9° NNW | 2026-02-05 09:34:37.816Z | 9.757° NNE | 17.353° | 2026-02-05 09:36:37.816Z | 42.301° NE |
| 4 mins | 2026-02-05 11:12:37.816Z | 340.69° N | 2026-02-05 11:14:37.816Z | 34.232° NE | 25.586° | 2026-02-05 11:16:37.816Z | 73.58° E |
| 5 mins | 2026-02-05 12:51:37.816Z | 289.631° WNW | 2026-02-05 12:53:37.816Z | 205.324° SW | 41.289° | 2026-02-05 12:56:37.816Z | 139.43° 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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