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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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
LTZH
Mission
Operational Commercial Communications
Bus & Motor
GUANGCHUAN, Unknown motor
Mass
~250 kg wet, ~250 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 26308.16400704 .00001952 00000-0 12046-3 0 9997
2 62112 49.9413 200.5484 0005946 191.3463 168.7355 15.14596032107399Epoch: 2026-11-04T03:56Z
TLE epoch observation values (Epoch: 2026-11-04T03:56:10.208Z)
Latitude
0.00004°
Longitude
98.08965°
Altitude
526.774 km
Speed
7.599 km/s
True Right ascension
13h 22m 11s
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
05:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.087 km
Perigee altitude
518.88 km
Semi-major axis
6,901.121 km
Eccentricity
0.00059
Inclination
49.9413°
RAAN
200.5484°
Arg. of periapsis
191.3463°
True anomaly
168.7488°
Mean anomaly
168.7355°
Eccentric anomaly
168.74215°
Mean motion
3.78585 °/min
Orbital period
95.09 mins
BSTAR
0.00012046
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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 | 2026-11-04 19:58:35.963Z | 225.298° WSW | 2026-11-04 20:00:35.963Z | 170.858° S | 74.351° | 2026-11-04 20:04:35.963Z | 58.507° ENE |
| 5 mins | 2026-11-04 21:38:35.963Z | 301.688° NW | 2026-11-04 21:40:35.963Z | 349.567° N | 27.281° | 2026-11-04 21:43:35.963Z | 40.35° NE |
| 4 mins | 2026-11-04 23:18:35.963Z | 327.383° NNW | 2026-11-04 23:20:35.963Z | 3.958° NNE | 19.091° | 2026-11-04 23:22:35.963Z | 39.356° NE |
| 5 mins | 2026-11-05 00:58:35.963Z | 331.961° NNW | 2026-11-05 01:00:35.963Z | 21.498° NNE | 33.217° | 2026-11-05 01:03:35.963Z | 83.308° E |
| 6 mins | 2026-11-05 02:37:35.963Z | 288.105° WNW | 2026-11-05 02:39:35.963Z | 242.588° WSW | 48.612° | 2026-11-05 02:43:35.963Z | 144.753° SSE |
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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