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: 6 hours ago
TLE from 6 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25310.94433432 .00006629 00000-0 36284-3 0 9995
2 62112 49.9415 165.2648 0007507 168.9539 191.1578 15.15288887 52471Epoch: 2025-11-06T22:39Z
TLE epoch observation values (Epoch: 2025-11-06T22:39:50.485Z)
Latitude
-0°
Longitude
138.90906°
Altitude
525.727 km
Speed
7.599 km/s
True Right ascension
11h 01m 03s
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
01:04:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.059 km
Perigee altitude
515.701 km
Semi-major axis
6,899.017 km
Eccentricity
0.00075
Inclination
49.9415°
RAAN
165.2648°
Arg. of periapsis
168.9539°
True anomaly
191.14117°
Mean anomaly
191.1578°
Eccentric anomaly
191.14948°
Mean motion
3.78758 °/min
Orbital period
95.05 mins
BSTAR
0.00036284
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-07 16:14:24.989Z | 168.328° S | 2025-11-07 16:16:24.989Z | 130.867° SE | 18.707° | 2025-11-07 16:18:24.989Z | 94.784° ESE |
| 6 mins | 2025-11-07 17:52:24.989Z | 249.186° W | 2025-11-07 17:55:24.989Z | 350.003° N | 41.858° | 2025-11-07 17:58:24.989Z | 49.709° ENE |
| 4 mins | 2025-11-07 19:33:24.989Z | 315.41° NNW | 2025-11-07 19:35:24.989Z | 358.511° N | 20.338° | 2025-11-07 19:37:24.989Z | 33.45° NE |
| 4 mins | 2025-11-07 21:13:24.989Z | 334.637° NNW | 2025-11-07 21:15:24.989Z | 14.218° NNE | 19.021° | 2025-11-07 21:17:24.989Z | 49.729° ENE |
| 6 mins | 2025-11-07 22:52:24.989Z | 318.746° NNW | 2025-11-07 22:55:24.989Z | 48.746° ENE | 35.85° | 2025-11-07 22:58:24.989Z | 101.937° ESE |
| 5 mins | 2025-11-08 00:32:24.989Z | 264.196° W | 2025-11-08 00:34:24.989Z | 214.571° SW | 24.723° | 2025-11-08 00:37:24.989Z | 165.104° S |
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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