Showing default

GEESAT 6-10, 65722

Orbit data source: Space-Track

GEESAT 6-10, 65722 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Wed, 24 Sep 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
65722, 2025-214L
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)
2025-09-24 (9 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, 1.1 m
Radar Cross Section
0.833 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 GEESAT 6-10
1 65722U 25214L   26171.36331169  .00000992  00000-0  14706-3 0  9996
2 65722  49.9910 294.0058 0011947 245.4153 114.5540 14.83380602 39973
Epoch: 2026-06-20T08:43Z
TLE epoch observation values (Epoch: 2026-06-20T08:43:10.130Z)
Latitude
-0.00008°
Longitude
-105.36548°
Altitude
622.698 km
Speed
7.547 km/s
True Right ascension
19h 36m 01s
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
07:12:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.793 km
Perigee altitude
611.073 km
Semi-major axis
6,997.57 km
Eccentricity
0.00119
Inclination
49.991°
RAAN
294.0058°
Arg. of periapsis
245.4153°
True anomaly
114.67845°
Mean anomaly
114.554°
Eccentric anomaly
114.61623°
Mean motion
3.70785 °/min
Orbital period
97.09 mins
BSTAR
0.00014706
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
|