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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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: 1 day ago
TLE from 1 day ago
0 GUANGCHUAN 02
1 62112U 24221B 26175.23167441 .00002688 00000-0 15956-3 0 9995
2 62112 49.9418 127.7966 0006746 13.8063 346.3071 15.14648296 87242Epoch: 2026-06-24T05:33Z
TLE epoch observation values (Epoch: 2026-06-24T05:33:36.669Z)
Latitude
0.00001°
Longitude
132.00197°
Altitude
518.07 km
Speed
7.608 km/s
True Right ascension
08h 31m 11s
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
16:18:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.48 km
Perigee altitude
518.169 km
Semi-major axis
6,900.962 km
Eccentricity
0.00067
Inclination
49.9418°
RAAN
127.7966°
Arg. of periapsis
13.8063°
True anomaly
346.28879°
Mean anomaly
346.3071°
Eccentric anomaly
346.29794°
Mean motion
3.78598 °/min
Orbital period
95.09 mins
BSTAR
0.00015956
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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 | 2026-06-25 05:46:58.239Z | 306.523° NW | 2026-06-25 05:50:58.239Z | 81.701° E | 43.445° | 2026-06-25 05:53:58.239Z | 119.088° SE |
| 5 mins | 2026-06-25 22:54:58.239Z | 193.26° SSW | 2026-06-25 22:56:58.239Z | 134.949° SE | 32.608° | 2026-06-25 22:59:58.239Z | 72.145° E |
| 5 mins | 2026-06-26 00:33:58.239Z | 278.579° WNW | 2026-06-26 00:35:58.239Z | 328.596° NNW | 31.381° | 2026-06-26 00:38:58.239Z | 39.118° NE |
| 4 mins | 2026-06-26 02:14:58.239Z | 331.386° NNW | 2026-06-26 02:15:58.239Z | 351.035° N | 18.208° | 2026-06-26 02:18:58.239Z | 41.75° NE |
| 4 mins | 2026-06-26 03:54:58.239Z | 343.132° N | 2026-06-26 03:55:58.239Z | 5.197° NNE | 22.589° | 2026-06-26 03:58:58.239Z | 65.939° ENE |
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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