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: 22 hours ago
TLE from 22 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26163.22427081 .00002653 00000-0 15796-3 0 9994
2 62112 49.9412 186.2547 0006968 324.9839 35.0653 15.14574954 85429Epoch: 2026-06-12T05:22Z
TLE epoch observation values (Epoch: 2026-06-12T05:22:56.997Z)
Latitude
-0.00001°
Longitude
-155.03958°
Altitude
518.88 km
Speed
7.608 km/s
True Right ascension
12h 25m 01s
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
14:03:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.856 km
Perigee altitude
518.239 km
Semi-major axis
6,901.185 km
Eccentricity
0.0007
Inclination
49.9412°
RAAN
186.2547°
Arg. of periapsis
324.9839°
True anomaly
35.11121°
Mean anomaly
35.0653°
Eccentric anomaly
35.08825°
Mean motion
3.7858 °/min
Orbital period
95.09 mins
BSTAR
0.00015796
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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 | 2026-06-13 03:42:52.923Z | 197.064° SSW | 2026-06-13 03:45:52.923Z | 137.074° SSE | 28.306° | 2026-06-13 03:48:52.923Z | 76.636° E |
| 5 mins | 2026-06-13 05:22:52.923Z | 272.08° WNW | 2026-06-13 05:24:52.923Z | 325.152° NNW | 34.387° | 2026-06-13 05:27:52.923Z | 40.967° NE |
| 4 mins | 2026-06-13 07:03:52.923Z | 329.655° NNW | 2026-06-13 07:04:52.923Z | 349.778° N | 18.825° | 2026-06-13 07:07:52.923Z | 40.583° NE |
| 4 mins | 2026-06-13 08:43:52.923Z | 342.903° N | 2026-06-13 08:44:52.923Z | 4.09° NNE | 21.445° | 2026-06-13 08:47:52.923Z | 62.211° ENE |
| 6 mins | 2026-06-13 10:22:52.923Z | 310.995° NW | 2026-06-13 10:24:52.923Z | 8.707° NNE | 43.777° | 2026-06-13 10:28:52.923Z | 118.603° SE |
| 6 mins | 2026-06-14 03:28:52.923Z | 197.45° SSW | 2026-06-14 03:30:52.923Z | 154.065° SSE | 31.12° | 2026-06-14 03:34:52.923Z | 69.79° E |
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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