GUANGCHUAN 02, 62112
Orbit data source: Space-Track
GUANGCHUAN 02, 62112 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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62112 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: 13 hours ago
TLE from 13 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26236.44663722 .00002284 00000-0 13662-3 0 9993
2 62112 49.9413 189.6689 0006497 267.0594 92.9613 15.15014187 96525Epoch: 2026-08-24T10:43Z
TLE epoch observation values (Epoch: 2026-08-24T10:43:09.455Z)
Latitude
-0.00005°
Longitude
56.15124°
Altitude
521.715 km
Speed
7.604 km/s
True Right ascension
12h 38m 40s
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
14:55:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.197 km
Perigee altitude
517.231 km
Semi-major axis
6,899.851 km
Eccentricity
0.00065
Inclination
49.9413°
RAAN
189.6689°
Arg. of periapsis
267.0594°
True anomaly
93.03565°
Mean anomaly
92.9613°
Eccentric anomaly
92.99847°
Mean motion
3.7869 °/min
Orbital period
95.06 mins
BSTAR
0.00013662
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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 02 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 | 2026-08-25 01:12:52.150Z | 274.165° WNW | 2026-08-25 01:15:52.150Z | 340.372° N | 30.257° | 2026-08-25 01:18:52.150Z | 40.613° NE |
| 5 mins | 2026-08-25 04:33:52.150Z | 331.829° NNW | 2026-08-25 04:35:52.150Z | 13.648° NNE | 23.878° | 2026-08-25 04:38:52.150Z | 71.176° E |
| 6 mins | 2026-08-25 06:12:52.150Z | 302.169° NW | 2026-08-25 06:15:52.150Z | 150.559° SSE | 43.986° | 2026-08-25 06:18:52.150Z | 128.347° SE |
| 6 mins | 2026-08-25 23:18:52.150Z | 211.263° SW | 2026-08-25 23:21:52.150Z | 115.797° SE | 37.373° | 2026-08-25 23:24:52.150Z | 65.533° ENE |
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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