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 26035.65713470 .00005999 00000-0 31859-3 0 9993
2 62112 49.9412 87.6192 0006624 178.0936 182.0041 15.16542417 66080Epoch: 2026-02-04T15:46Z
TLE epoch observation values (Epoch: 2026-02-04T15:46:16.438Z)
Latitude
-0.00005°
Longitude
76.23009°
Altitude
521.409 km
Speed
7.601 km/s
True Right ascension
05h 50m 28s
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
521.646 km
Perigee altitude
512.512 km
Semi-major axis
6,895.216 km
Eccentricity
0.00066
Inclination
49.9412°
RAAN
87.6192°
Arg. of periapsis
178.0936°
True anomaly
182.00145°
Mean anomaly
182.0041°
Eccentric anomaly
182.00277°
Mean motion
3.79072 °/min
Orbital period
94.97 mins
BSTAR
0.00031859
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-05 06:10:37.521Z | 221.51° SW | 2026-02-05 06:14:37.521Z | 116.656° SE | 40.477° | 2026-02-05 06:17:37.521Z | 63.21° ENE |
| 5 mins | 2026-02-05 07:51:37.521Z | 291.761° WNW | 2026-02-05 07:53:37.521Z | 338.901° N | 26.585° | 2026-02-05 07:56:37.521Z | 38.337° NE |
| 5 mins | 2026-02-05 11:11:37.521Z | 332.297° NNW | 2026-02-05 11:13:37.521Z | 18.675° NNE | 26.245° | 2026-02-05 11:16:37.521Z | 78.462° E |
| 6 mins | 2026-02-05 12:50:37.521Z | 293.44° NW | 2026-02-05 12:52:37.521Z | 249.986° W | 40.359° | 2026-02-05 12:56:37.521Z | 137.914° SSE |
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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