Showing default

GJZ 03, 62292

Orbit data source: Space-Track

GJZ 03, 62292 is a payload satellite owned by CASC (CN) in LEO that was launched on Thu, 12 Dec 2024 UTC via a CHANG ZHENG 2D/YZ-3 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
62292, 2024-238C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
HITSAT
Mission
Operational Civil Communications
Bus & Motor
HARBFLAT, Unknown motor
Mass
~150 kg wet, ~150 kg dry
Launch date (UTC)
2024-12-12 (9 months ago)
Launch vehicle
CHANG ZHENG 2D/YZ-3
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.5 m
Radar Cross Section
0.240 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 GJZ 03
1 62292U 24238C   25253.20658543 -.00000080  00000-0  40744-4 0  9992
2 62292  59.9143  38.4314 0027838 113.1951 247.1993 13.75149355 37385
Epoch: 2025-09-10T04:57Z
TLE epoch observation values (Epoch: 2025-09-10T04:57:28.981Z)
Latitude
-0.00002°
Longitude
-25.42569°
Altitude
990.615 km
Speed
7.353 km/s
True Right ascension
02h 33m 43s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:04:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,000.895 km
Perigee altitude
959.925 km
Semi-major axis
7,358.547 km
Eccentricity
0.00278
Inclination
59.9143°
RAAN
38.4314°
Arg. of periapsis
113.1951°
True anomaly
246.90562°
Mean anomaly
247.1993°
Eccentric anomaly
247.05242°
Mean motion
3.43839 °/min
Orbital period
104.7 mins
BSTAR
0.000040744
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 #238 in the year 2024 (2024-12-12 UTC)

Documentation

Showing up to 5 results
|