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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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: 14 hours ago
TLE from 14 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25298.41411770 .00007967 00000-0 43472-3 0 9996
2 62112 49.9430 226.3219 0007334 116.8777 243.2924 15.15128884 50578Epoch: 2025-10-25T09:56Z
TLE epoch observation values (Epoch: 2025-10-25T09:56:19.769Z)
Latitude
-0.00002°
Longitude
43.1945°
Altitude
523.41 km
Speed
7.602 km/s
True Right ascension
15h 05m 17s
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
19:14:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.426 km
Perigee altitude
516.305 km
Semi-major axis
6,899.503 km
Eccentricity
0.00073
Inclination
49.943°
RAAN
226.3219°
Arg. of periapsis
116.8777°
True anomaly
243.21736°
Mean anomaly
243.2924°
Eccentric anomaly
243.25487°
Mean motion
3.78718 °/min
Orbital period
95.06 mins
BSTAR
0.00043472
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-26 00:29:07.904Z | 302.03° NW | 2025-10-26 00:31:07.904Z | 338.3° N | 20.678° | 2025-10-26 00:34:07.904Z | 35.152° NE |
| 4 mins | 2025-10-26 02:10:07.904Z | 336.748° NNW | 2025-10-26 02:12:07.904Z | 16.968° NNE | 18.556° | 2025-10-26 02:14:07.904Z | 50.86° ENE |
| 6 mins | 2025-10-26 03:49:07.904Z | 320.709° NNW | 2025-10-26 03:51:07.904Z | 3.788° NNE | 34.483° | 2025-10-26 03:55:07.904Z | 100.878° ESE |
| 4 mins | 2025-10-26 05:29:07.904Z | 263.696° W | 2025-10-26 05:31:07.904Z | 210.726° SW | 25.694° | 2025-10-26 05:33:07.904Z | 171.479° S |
| 4 mins | 2025-10-26 20:56:07.904Z | 166.408° S | 2025-10-26 20:58:07.904Z | 124.769° SE | 19.874° | 2025-10-26 21:00:07.904Z | 89.798° E |
| 6 mins | 2025-10-26 22:34:07.904Z | 253.773° W | 2025-10-26 22:37:07.904Z | 3.843° NNE | 39.343° | 2025-10-26 22:40:07.904Z | 49.295° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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