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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Edit Public Description
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 26038.16094312 .00007478 00000-0 39276-3 0 9994
2 62112 49.9414 75.3922 0006568 187.3580 172.7276 15.16578888 66461Epoch: 2026-02-07T03:51Z
TLE epoch observation values (Epoch: 2026-02-07T03:51:45.485Z)
Latitude
-0.00002°
Longitude
-119.83578°
Altitude
521.227 km
Speed
7.602 km/s
True Right ascension
05h 01m 34s
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
11:52:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.497 km
Perigee altitude
512.44 km
Semi-major axis
6,895.105 km
Eccentricity
0.00066
Inclination
49.9414°
RAAN
75.3922°
Arg. of periapsis
187.358°
True anomaly
172.73712°
Mean anomaly
172.7276°
Eccentric anomaly
172.73236°
Mean motion
3.79081 °/min
Orbital period
94.97 mins
BSTAR
0.00039276
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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 | 2026-02-07 10:37:31.198Z | 318.81° NNW | 2026-02-07 10:40:31.198Z | 15.091° NNE | 28.931° | 2026-02-07 10:43:31.198Z | 83.04° E |
| 6 mins | 2026-02-07 12:17:31.198Z | 286.936° WNW | 2026-02-07 12:19:31.198Z | 242.699° WSW | 35.421° | 2026-02-07 12:23:31.198Z | 146.502° SSE |
| 6 mins | 2026-02-08 05:22:31.198Z | 233.667° WSW | 2026-02-08 05:24:31.198Z | 225.192° WSW | 44.432° | 2026-02-08 05:28:31.198Z | 56.312° ENE |
| 5 mins | 2026-02-08 07:02:31.198Z | 304.798° NW | 2026-02-08 07:04:31.198Z | 350.623° N | 23.039° | 2026-02-08 07:07:31.198Z | 40.66° NE |
| 4 mins | 2026-02-08 08:42:31.198Z | 330.328° NNW | 2026-02-08 08:44:31.198Z | 8.131° NNE | 18.03° | 2026-02-08 08:46:31.198Z | 43.212° NE |
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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