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: 6 hours ago
TLE from 6 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26093.27827781 .00007405 00000-0 41713-3 0 9990
2 62112 49.9421 166.6339 0006176 41.3366 318.8051 15.14092824 74823Epoch: 2026-04-03T06:40Z
TLE epoch observation values (Epoch: 2026-04-03T06:40:43.202Z)
Latitude
-0.00002°
Longitude
-125.16083°
Altitude
521.073 km
Speed
7.606 km/s
True Right ascension
11h 06m 32s
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
18:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.775 km
Perigee altitude
520.249 km
Semi-major axis
6,902.649 km
Eccentricity
0.00062
Inclination
49.9421°
RAAN
166.6339°
Arg. of periapsis
41.3366°
True anomaly
318.75846°
Mean anomaly
318.8051°
Eccentric anomaly
318.78178°
Mean motion
3.7846 °/min
Orbital period
95.12 mins
BSTAR
0.00041713
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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 | 2026-04-03 13:28:22.646Z | 317.15° NNW | 2026-04-03 13:31:22.646Z | 26.581° NE | 35.328° | 2026-04-03 13:34:22.646Z | 96.725° ESE |
| 5 mins | 2026-04-03 15:08:22.646Z | 273.966° WNW | 2026-04-03 15:10:22.646Z | 229.447° WSW | 27.173° | 2026-04-03 15:13:22.646Z | 166.425° S |
| 4 mins | 2026-04-04 06:36:22.646Z | 170.072° S | 2026-04-04 06:38:22.646Z | 131.04° SE | 19.701° | 2026-04-04 06:40:22.646Z | 93.736° ESE |
| 6 mins | 2026-04-04 08:14:22.646Z | 251.214° W | 2026-04-04 08:17:22.646Z | 339.758° N | 41.17° | 2026-04-04 08:20:22.646Z | 48.382° ENE |
| 4 mins | 2026-04-04 09:55:22.646Z | 313.31° NW | 2026-04-04 09:57:22.646Z | 354.634° N | 20.244° | 2026-04-04 09:59:22.646Z | 31.292° NE |
| 4 mins | 2026-04-04 11:36:22.646Z | 347.737° N | 2026-04-04 11:37:22.646Z | 8.894° NNE | 19.467° | 2026-04-04 11:40:22.646Z | 58.973° ENE |
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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