Showing default

GEESAT 4-02, 65120

Orbit data source: Space-Track

GEESAT 4-02, 65120 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 08 Aug 2025 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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
65120, 2025-170B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
2025-08-08 (8 months ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 GEESAT 4-02
1 65120U 25170B   26095.62775963  .00002848  00000-0  36531-3 0  9999
2 65120  49.9836 150.7631 0009484 169.8973 190.2157 14.83994668 35681
Epoch: 2026-04-05T15:03Z
TLE epoch observation values (Epoch: 2026-04-05T15:03:58.432Z)
Latitude
-0.00003°
Longitude
90.83914°
Altitude
623.814 km
Speed
7.545 km/s
True Right ascension
10h 03m 03s
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
11:45:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.139 km
Perigee altitude
610.87 km
Semi-major axis
6,995.641 km
Eccentricity
0.00095
Inclination
49.9836°
RAAN
150.7631°
Arg. of periapsis
169.8973°
True anomaly
190.19645°
Mean anomaly
190.2157°
Eccentric anomaly
190.20607°
Mean motion
3.70938 °/min
Orbital period
97.05 mins
BSTAR
0.00036531
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...

Documentation

Showing up to 5 results
|