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GEESAT 4-09, 65127

Orbit data source: Space-Track

GEESAT 4-09, 65127 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.

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Identifier
65127, 2025-170J
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, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)

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

TLE from 4 days ago
0 GEESAT 4-09
1 65127U 25170J   26155.26697449  .00001821  00000-0  25839-3 0  9994
2 65127  49.9920 263.6232 0021928 340.6598  19.3505 14.81340956 44087
Epoch: 2026-06-04T06:24Z
TLE epoch observation values (Epoch: 2026-06-04T06:24:26.595Z)
Latitude
-0.00005°
Longitude
-85.20135°
Altitude
611.153 km
Speed
7.563 km/s
True Right ascension
17h 34m 29s
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
10:48:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.212 km
Perigee altitude
610.495 km
Semi-major axis
7,003.99 km
Eccentricity
0.00219
Inclination
49.992°
RAAN
263.6232°
Arg. of periapsis
340.6598°
True anomaly
19.43398°
Mean anomaly
19.3505°
Eccentric anomaly
19.39222°
Mean motion
3.70275 °/min
Orbital period
97.22 mins
BSTAR
0.00025839
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