GUANGCHUAN 02, 62112
Orbit data source: Space-Track
GUANGCHUAN 02, 62112 is a Chinese payload satellite 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: 17 hours ago
TLE from 17 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25260.22020780 .00005234 00000-0 29619-3 0 9993
2 62112 49.9432 52.3225 0007041 319.4788 40.5638 15.14520378 44781Epoch: 2025-09-17T05:17Z
TLE epoch observation values (Epoch: 2025-09-17T05:17:05.953Z)
Latitude
-0.00001°
Longitude
-23.3516°
Altitude
519.291 km
Speed
7.607 km/s
True Right ascension
03h 29m 17s
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
14:51:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.072 km
Perigee altitude
518.354 km
Semi-major axis
6,901.35 km
Eccentricity
0.0007
Inclination
49.9432°
RAAN
52.3225°
Arg. of periapsis
319.4788°
True anomaly
40.6163°
Mean anomaly
40.5638°
Eccentric anomaly
40.59005°
Mean motion
3.78566 °/min
Orbital period
95.1 mins
BSTAR
0.00029619
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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 | 2025-09-18 13:09:48.934Z | 235.737° WSW | 2025-09-18 13:11:48.934Z | 238.892° WSW | 42.838° | 2025-09-18 13:15:48.934Z | 55.595° ENE |
| 5 mins | 2025-09-18 14:49:48.934Z | 299.723° NW | 2025-09-18 14:51:48.934Z | 340.613° N | 23.006° | 2025-09-18 14:54:48.934Z | 36.944° NE |
| 4 mins | 2025-09-18 16:30:48.934Z | 337.964° N | 2025-09-18 16:31:48.934Z | 357.076° N | 18.269° | 2025-09-18 16:34:48.934Z | 49.213° ENE |
| 6 mins | 2025-09-18 18:09:48.934Z | 324.896° NNW | 2025-09-18 18:11:48.934Z | 8.595° NNE | 31.083° | 2025-09-18 18:15:48.934Z | 93.551° ESE |
| 6 mins | 2025-09-18 19:48:48.934Z | 284.721° WNW | 2025-09-18 19:51:48.934Z | 208.52° SW | 32.375° | 2025-09-18 19:54:48.934Z | 154.006° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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