Showing default

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.

Loading next visibility...
Identifier
62112, 2024-221B
Orbit
LEO
Last TLE update
16 hours ago
Origin
Manufacturer
CAST?
Mission
Operational Commercial Communications
Bus & Motor
HQ, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
2024-11-27 (7 months ago)
Launch vehicle
ZHUQUE-2E
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 6 m
Radar Cross Section
4.560 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago
0 GUANGCHUAN 02
1 62112U 24221B   25191.72367180  .00002047  00000-0  12680-3 0  9998
2 62112  49.9448  25.6144 0008332  44.8871 315.2752 15.14229010 34403
Epoch: 2025-07-10T17:22Z
TLE epoch observation values (Epoch: 2025-07-10T17:22:05.243Z)
Latitude
-0.00002°
Longitude
-163.79331°
Altitude
519.783 km
Speed
7.607 km/s
True Right ascension
01h 42m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
10.2054°
Longitude
-158.36013°
Altitude
518.348 km
Speed
7.609 km/s
Apparent Right ascension
04h 54m 37s
Apparent Declination
-23° 06' 42"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:33:33
Azimuth
96.389° ESE
Elevation
-29.751°
Doppler factor
1
Orbital elements
Apogee altitude
529.849 km
Perigee altitude
518.347 km
Semi-major axis
6,902.235 km
Eccentricity
0.00083
Inclination
49.9448°
RAAN
25.6144°
Arg. of periapsis
44.8871°
True anomaly
Unknown
Mean anomaly
315.2752°
Eccentric anomaly
Unknown
Mean motion
3.78494 °/min
Orbital period
95.11 mins
BSTAR
0.0001268
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
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)

GUANGCHUAN 02 Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-07-11 15:42:52.109Z224.598° SW2025-07-11 15:46:52.109Z128.432° SE42.398°2025-07-11 15:49:52.109Z62.095° ENE
5 mins2025-07-11 17:23:52.109Z289.001° WNW2025-07-11 17:25:52.109Z329.182° NNW25.315°2025-07-11 17:28:52.109Z34.507° NE
4 mins2025-07-11 19:04:52.109Z331.101° NNW2025-07-11 19:06:52.109Z9.734° NNE17.626°2025-07-11 19:08:52.109Z42.641° NE
5 mins2025-07-11 20:44:52.109Z337.039° NNW2025-07-11 20:46:52.109Z29.994° NE27.166°2025-07-11 20:49:52.109Z83.295° E
6 mins2025-07-11 22:23:52.109Z289.168° WNW2025-07-11 22:25:52.109Z231.057° WSW39.735°2025-07-11 22:29:52.109Z140.458° SSE
|