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: 7 hours ago
TLE from 7 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26125.94443794 .00004244 00000-0 24458-3 0 9993
2 62112 49.9440 7.7001 0006450 175.9430 184.1573 15.14328966 79777Epoch: 2026-05-05T22:39Z
TLE epoch observation values (Epoch: 2026-05-05T22:39:59.438Z)
Latitude
-0.00006°
Longitude
163.89038°
Altitude
528.001 km
Speed
7.598 km/s
True Right ascension
00h 30m 48s
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
13:35:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.246 km
Perigee altitude
519.343 km
Semi-major axis
6,901.931 km
Eccentricity
0.00065
Inclination
49.944°
RAAN
7.7001°
Arg. of periapsis
175.943°
True anomaly
184.15195°
Mean anomaly
184.1573°
Eccentric anomaly
184.15462°
Mean motion
3.78519 °/min
Orbital period
95.11 mins
BSTAR
0.00024458
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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 | 2026-05-06 17:49:26.782Z | 175.804° S | 2026-05-06 17:52:26.782Z | 124.695° SE | 17.752° | 2026-05-06 17:54:26.782Z | 91.84° ESE |
| 6 mins | 2026-05-06 19:28:26.782Z | 248.246° W | 2026-05-06 19:31:26.782Z | 12.319° NNE | 41.159° | 2026-05-06 19:34:26.782Z | 51.11° ENE |
| 4 mins | 2026-05-06 21:09:26.782Z | 318.122° NNW | 2026-05-06 21:10:26.782Z | 339.267° N | 20.912° | 2026-05-06 21:13:26.782Z | 35.521° NE |
| 4 mins | 2026-05-06 22:49:26.782Z | 336.423° NNW | 2026-05-06 22:51:26.782Z | 16.488° NNE | 18.846° | 2026-05-06 22:53:26.782Z | 50.631° ENE |
| 6 mins | 2026-05-07 00:28:26.782Z | 319.841° NNW | 2026-05-07 00:31:26.782Z | 49.423° ENE | 35.013° | 2026-05-07 00:34:26.782Z | 100.782° ESE |
| 5 mins | 2026-05-07 02:08:26.782Z | 265.776° W | 2026-05-07 02:10:26.782Z | 214.986° SW | 25.862° | 2026-05-07 02:13:26.782Z | 163.97° S |
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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