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: 10 hours ago
TLE from 10 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26305.92084149 .00001661 00000-0 10499-3 0 9996
2 62112 49.9416 211.4688 0005929 182.7642 177.3277 15.14587326107051Epoch: 2026-11-01T22:06Z
TLE epoch observation values (Epoch: 2026-11-01T22:06:00.704Z)
Latitude
-0.00001°
Longitude
-161.23942°
Altitude
526.863 km
Speed
7.599 km/s
True Right ascension
14h 05m 52s
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
04:08:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.102 km
Perigee altitude
518.918 km
Semi-major axis
6,901.147 km
Eccentricity
0.00059
Inclination
49.9416°
RAAN
211.4688°
Arg. of periapsis
182.7642°
True anomaly
177.33087°
Mean anomaly
177.3277°
Eccentric anomaly
177.32928°
Mean motion
3.78583 °/min
Orbital period
95.09 mins
BSTAR
0.00010499
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-02 20:26:01.882Z | 218.347° SW | 2026-11-02 20:30:01.882Z | 133.997° SE | 54.642° | 2026-11-02 20:33:01.882Z | 66.096° ENE |
| 5 mins | 2026-11-02 22:07:01.882Z | 285.258° WNW | 2026-11-02 22:09:01.882Z | 328.378° NNW | 31.736° | 2026-11-02 22:12:01.882Z | 35.653° NE |
| 4 mins | 2026-11-02 23:48:01.882Z | 331.106° NNW | 2026-11-02 23:49:01.882Z | 349.58° N | 18.731° | 2026-11-02 23:52:01.882Z | 41.628° NE |
| 5 mins | 2026-11-03 01:28:01.882Z | 339.778° N | 2026-11-03 01:30:01.882Z | 29.608° NE | 27.727° | 2026-11-03 01:33:01.882Z | 79.161° E |
| 6 mins | 2026-11-03 03:07:01.882Z | 296.141° NW | 2026-11-03 03:09:01.882Z | 237.307° WSW | 70.113° | 2026-11-03 03:13:01.882Z | 133.501° SE |
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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