Showing default

GEESAT 4-08, 65126

Orbit data source: Space-Track

GEESAT 4-08, 65126 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
65126, 2025-170H
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 (6 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: 17 hours ago

TLE from 17 hours ago
0 GEESAT 4-08
1 65126U 25170H   26034.56906657  .00042924  00000-0  94749-3 0  9991
2 65126  49.9764  41.1817 0009523 157.7021 202.4358 15.43359669 27021
Epoch: 2026-02-03T13:39Z
TLE epoch observation values (Epoch: 2026-02-03T13:39:27.351Z)
Latitude
-0.00001°
Longitude
62.56961°
Altitude
442.757 km
Speed
7.644 km/s
True Right ascension
02h 44m 43s
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
08:36:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.474 km
Perigee altitude
430.494 km
Semi-major axis
6,815.121 km
Eccentricity
0.00095
Inclination
49.9764°
RAAN
41.1817°
Arg. of periapsis
157.7021°
True anomaly
202.3942°
Mean anomaly
202.4358°
Eccentric anomaly
202.41499°
Mean motion
3.85774 °/min
Orbital period
93.32 mins
BSTAR
0.00094749
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
|