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: 7 hours ago
TLE from 7 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 26306.11876838 .00001680 00000-0 10597-3 0 9992
2 62112 49.9415 210.5053 0005925 183.4952 176.5958 15.14588072107083Epoch: 2026-11-02T02:51Z
TLE epoch observation values (Epoch: 2026-11-02T02:51:01.588Z)
Latitude
-0°
Longitude
126.34831°
Altitude
526.856 km
Speed
7.599 km/s
True Right ascension
14h 02m 01s
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
05:13:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.097 km
Perigee altitude
518.919 km
Semi-major axis
6,901.145 km
Eccentricity
0.00059
Inclination
49.9415°
RAAN
210.5053°
Arg. of periapsis
183.4952°
True anomaly
176.59983°
Mean anomaly
176.5958°
Eccentric anomaly
176.59781°
Mean motion
3.78583 °/min
Orbital period
95.09 mins
BSTAR
0.00010597
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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 20:26:50.343Z | 215.382° SW | 2026-11-02 20:29:50.343Z | 147.141° SSE | 54.654° | 2026-11-02 20:33:50.343Z | 63.17° ENE |
| 6 mins | 2026-11-02 22:06:50.343Z | 283.002° WNW | 2026-11-02 22:09:50.343Z | 354.09° N | 31.052° | 2026-11-02 22:12:50.343Z | 42.44° NE |
| 4 mins | 2026-11-02 23:47:50.343Z | 328.024° NNW | 2026-11-02 23:49:50.343Z | 6.077° NNE | 18.82° | 2026-11-02 23:51:50.343Z | 39.332° NE |
| 5 mins | 2026-11-03 01:27:50.343Z | 336.552° NNW | 2026-11-03 01:29:50.343Z | 24.21° NE | 28.104° | 2026-11-03 01:32:50.343Z | 77.59° E |
| 6 mins | 2026-11-03 03:06:50.343Z | 296.972° NW | 2026-11-03 03:08:50.343Z | 257.247° W | 65.992° | 2026-11-03 03:12:50.343Z | 133.793° 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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