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: 5 hours ago
TLE from 5 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26128.18797793 .00002853 00000-0 16974-3 0 9991
2 62112 49.9444 356.7824 0006541 185.4113 174.6768 15.14344396 80111Epoch: 2026-05-08T04:30Z
TLE epoch observation values (Epoch: 2026-05-08T04:30:41.293Z)
Latitude
0.00001°
Longitude
63.087°
Altitude
528.009 km
Speed
7.598 km/s
True Right ascension
23h 47m 07s
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
17:51:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.262 km
Perigee altitude
519.233 km
Semi-major axis
6,901.884 km
Eccentricity
0.00065
Inclination
49.9444°
RAAN
356.7824°
Arg. of periapsis
185.4113°
True anomaly
174.68375°
Mean anomaly
174.6768°
Eccentric anomaly
174.68027°
Mean motion
3.78522 °/min
Orbital period
95.11 mins
BSTAR
0.00016974
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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 | 2026-05-08 17:20:52.182Z | 183.528° SSW | 2026-05-08 17:22:52.182Z | 146.214° SSE | 23.416° | 2026-05-08 17:25:52.182Z | 84.717° E |
| 6 mins | 2026-05-08 18:59:52.182Z | 261.038° W | 2026-05-08 19:02:52.182Z | 359.502° N | 36.63° | 2026-05-08 19:05:52.182Z | 47.292° ENE |
| 4 mins | 2026-05-08 20:40:52.182Z | 321.74° NNW | 2026-05-08 20:41:52.182Z | 341.382° N | 19.307° | 2026-05-08 20:44:52.182Z | 36.11° NE |
| 4 mins | 2026-05-08 22:20:52.182Z | 336.956° NNW | 2026-05-08 22:22:52.182Z | 18.421° NNE | 20.261° | 2026-05-08 22:24:52.182Z | 54.697° ENE |
| 6 mins | 2026-05-08 23:59:52.182Z | 314.47° NW | 2026-05-09 00:02:52.182Z | 66.15° ENE | 39.572° | 2026-05-09 00:05:52.182Z | 110.739° ESE |
| 4 mins | 2026-05-09 01:39:52.182Z | 257.448° W | 2026-05-09 01:41:52.182Z | 215.673° SW | 19.456° | 2026-05-09 01:43:52.182Z | 182.039° SSW |
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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