Showing default

GEESAT 4-03, 65121

Orbit data source: Space-Track

GEESAT 4-03, 65121 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
65121, 2025-170C
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 (10 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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 GEESAT 4-03
1 65121U 25170C   26155.25748694  .00001958  00000-0  25929-3 0  9997
2 65121  49.9911 234.0557 0020318  10.9111 349.2264 14.84017321 44518
Epoch: 2026-06-04T06:10Z
TLE epoch observation values (Epoch: 2026-06-04T06:10:46.871Z)
Latitude
-0.00004°
Longitude
-111.34398°
Altitude
603.255 km
Speed
7.567 km/s
True Right ascension
15h 36m 13s
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
10:50:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.645 km
Perigee altitude
603.218 km
Semi-major axis
6,995.569 km
Eccentricity
0.00203
Inclination
49.9911°
RAAN
234.0557°
Arg. of periapsis
10.9111°
True anomaly
349.18277°
Mean anomaly
349.2264°
Eccentric anomaly
349.2046°
Mean motion
3.70944 °/min
Orbital period
97.05 mins
BSTAR
0.00025929
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
|