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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
62112 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
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: 9 hours ago
TLE from 9 hours ago
0 GUANGCHUAN 02
1 62112U 24221B 25260.87999291 .00005082 00000-0 28803-3 0 9991
2 62112 49.9442 49.1109 0007060 322.3119 37.7336 15.14527221 44887Epoch: 2025-09-17T21:07Z
TLE epoch observation values (Epoch: 2025-09-17T21:07:11.387Z)
Latitude
-0.00003°
Longitude
95.26383°
Altitude
519.108 km
Speed
7.607 km/s
True Right ascension
03h 16m 26s
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
23:05:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.064 km
Perigee altitude
518.32 km
Semi-major axis
6,901.329 km
Eccentricity
0.00071
Inclination
49.9442°
RAAN
49.1109°
Arg. of periapsis
322.3119°
True anomaly
37.78315°
Mean anomaly
37.7336°
Eccentric anomaly
37.75837°
Mean motion
3.78568 °/min
Orbital period
95.1 mins
BSTAR
0.00028803
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #221 in the year 2024 (2024-11-27 UTC)
Did you know?
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
Loading observer location...
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 13:09:46.422Z | 235.719° WSW | 2025-09-18 13:12:46.422Z | 52.025° ENE | 42.827° | 2025-09-18 13:15:46.422Z | 55.579° ENE |
| 5 mins | 2025-09-18 14:49:46.422Z | 299.141° NW | 2025-09-18 14:51:46.422Z | 339.513° N | 22.975° | 2025-09-18 14:54:46.422Z | 36.507° NE |
| 4 mins | 2025-09-18 16:30:46.422Z | 337.241° NNW | 2025-09-18 16:31:46.422Z | 356.194° N | 18.22° | 2025-09-18 16:34:46.422Z | 48.725° ENE |
| 6 mins | 2025-09-18 18:09:46.422Z | 324.445° NNW | 2025-09-18 18:11:46.422Z | 7.034° NNE | 30.933° | 2025-09-18 18:15:46.422Z | 93.293° ESE |
| 6 mins | 2025-09-18 19:48:46.422Z | 285.088° WNW | 2025-09-18 19:51:46.422Z | 210.247° SW | 32.493° | 2025-09-18 19:54:46.422Z | 154.261° 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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|