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: 7 hours ago
TLE from 7 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25312.85671514 .00007348 00000-0 40003-3 0 9995
2 62112 49.9418 155.9445 0007577 177.2922 182.8071 15.15322726 52769Epoch: 2025-11-08T20:33Z
TLE epoch observation values (Epoch: 2025-11-08T20:33:40.188Z)
Latitude
-0.00001°
Longitude
159.24673°
Altitude
525.764 km
Speed
7.599 km/s
True Right ascension
10h 23m 46s
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
23:58:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.005 km
Perigee altitude
515.55 km
Semi-major axis
6,898.914 km
Eccentricity
0.00076
Inclination
49.9418°
RAAN
155.9445°
Arg. of periapsis
177.2922°
True anomaly
182.80285°
Mean anomaly
182.8071°
Eccentric anomaly
182.80498°
Mean motion
3.78767 °/min
Orbital period
95.05 mins
BSTAR
0.00040003
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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 | 2025-11-09 15:42:52.086Z | 187.891° SSW | 2025-11-09 15:45:52.086Z | 129.031° SE | 23.948° | 2025-11-09 15:48:52.086Z | 78.259° E |
| 6 mins | 2025-11-09 17:21:52.086Z | 259.521° W | 2025-11-09 17:24:52.086Z | 343.732° N | 37.566° | 2025-11-09 17:27:52.086Z | 45.776° ENE |
| 4 mins | 2025-11-09 19:02:52.086Z | 318.171° NNW | 2025-11-09 19:04:52.086Z | 358.542° N | 19.23° | 2025-11-09 19:06:52.086Z | 33.509° NE |
| 4 mins | 2025-11-09 20:42:52.086Z | 334.554° NNW | 2025-11-09 20:44:52.086Z | 15.002° NNE | 20.329° | 2025-11-09 20:46:52.086Z | 52.901° ENE |
| 6 mins | 2025-11-09 22:21:52.086Z | 313.759° NW | 2025-11-09 22:24:52.086Z | 61.885° ENE | 40.19° | 2025-11-09 22:27:52.086Z | 110.875° ESE |
| 4 mins | 2025-11-10 00:01:52.086Z | 257.471° W | 2025-11-10 00:03:52.086Z | 216.009° SW | 19.146° | 2025-11-10 00:05:52.086Z | 182.43° SSW |
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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