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: 9 hours ago
TLE from 9 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25296.69934869 .00007805 00000-0 42657-3 0 9998
2 62112 49.9428 234.6761 0007317 109.5590 250.6152 15.15100109 50319Epoch: 2025-10-23T16:47Z
TLE epoch observation values (Epoch: 2025-10-23T16:47:03.726Z)
Latitude
0.00001°
Longitude
-49.44427°
Altitude
522.899 km
Speed
7.602 km/s
True Right ascension
15h 38m 42s
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
20:30:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.501 km
Perigee altitude
516.404 km
Semi-major axis
6,899.59 km
Eccentricity
0.00073
Inclination
49.9428°
RAAN
234.6761°
Arg. of periapsis
109.559°
True anomaly
250.53613°
Mean anomaly
250.6152°
Eccentric anomaly
250.57566°
Mean motion
3.78711 °/min
Orbital period
95.06 mins
BSTAR
0.00042657
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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 | 2025-10-24 02:39:01.230Z | 319.078° NNW | 2025-10-24 02:42:01.230Z | 10.694° NNE | 17.98° | 2025-10-24 02:44:01.230Z | 45.022° ENE |
| 5 mins | 2025-10-24 04:20:01.230Z | 334.544° NNW | 2025-10-24 04:22:01.230Z | 35.832° NE | 30.885° | 2025-10-24 04:25:01.230Z | 91.382° ESE |
| 5 mins | 2025-10-24 05:59:01.230Z | 277.066° WNW | 2025-10-24 06:01:01.230Z | 218.679° SW | 32.847° | 2025-10-24 06:04:01.230Z | 154.969° SSE |
| 6 mins | 2025-10-24 23:04:01.230Z | 241.021° WSW | 2025-10-24 23:07:01.230Z | 359.758° N | 44.184° | 2025-10-24 23:10:01.230Z | 52.983° ENE |
| 4 mins | 2025-10-25 00:45:01.230Z | 312.083° NW | 2025-10-25 00:47:01.230Z | 357.43° N | 21.357° | 2025-10-25 00:49:01.230Z | 33.096° NE |
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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