Showing default

GEESAT 5-08, 65557

Orbit data source: Space-Track

GEESAT 5-08, 65557 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Mon, 08 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
65557, 2025-201H
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)
2025-09-08 (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: 14 hours ago

TLE from 14 hours ago
0 GEESAT 5-08
1 65557U 25201H   26171.30331080  .00001010  00000-0  15760-3 0  9997
2 65557  49.9816  21.3122 0009449 305.2267  54.7785 14.80944217 42315
Epoch: 2026-06-20T07:16Z
TLE epoch observation values (Epoch: 2026-06-20T07:16:46.053Z)
Latitude
Longitude
3.60045°
Altitude
623.074 km
Speed
7.551 km/s
True Right ascension
01h 25m 14s
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
08:42:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
633.725 km
Perigee altitude
620.486 km
Semi-major axis
7,005.243 km
Eccentricity
0.00094
Inclination
49.9816°
RAAN
21.3122°
Arg. of periapsis
305.2267°
True anomaly
54.86702°
Mean anomaly
54.7785°
Eccentric anomaly
54.82275°
Mean motion
3.70176 °/min
Orbital period
97.25 mins
BSTAR
0.0001576
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
|