Showing default

GJZ 02, 62291

Orbit data source: Space-Track

GJZ 02, 62291 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
62291, 2024-238B
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 (1 year 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 hours ago

TLE from 6 hours ago
0 GJZ 02
1 62291U 24238B   26126.24873362  .00000023  00000-0  14783-3 0  9992
2 62291  59.9201  17.6977 0007249  91.2185 268.9654 13.75198265 70513
Epoch: 2026-05-06T05:58Z
TLE epoch observation values (Epoch: 2026-05-06T05:58:10.584Z)
Latitude
0.00002°
Longitude
64.04167°
Altitude
982.553 km
Speed
7.361 km/s
True Right ascension
01h 10m 47s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
19:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
985.569 km
Perigee altitude
974.901 km
Semi-major axis
7,358.372 km
Eccentricity
0.00072
Inclination
59.9201°
RAAN
17.6977°
Arg. of periapsis
91.2185°
True anomaly
268.88235°
Mean anomaly
268.9654°
Eccentric anomaly
268.92387°
Mean motion
3.43851 °/min
Orbital period
104.7 mins
BSTAR
0.00014783
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
|