OBJECT G, 65556

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT G, 65556 is a 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). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.

Loading next visibility...
Identifier
65556, 2025-201G
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Taizhou Xingkong
Mission
Operational spacecraft
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
2025-09-08 (1 week ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 OBJECT G
1 65556U 25201G   25258.57138364  .00003308  00000-0  34979-3 0  9995
2 65556  49.9861 233.5897 0011961 318.2053  41.7975 14.91577636  1006
Epoch: 2025-09-15T13:42Z
TLE epoch observation values (Epoch: 2025-09-15T13:42:47.546Z)
Latitude
0.00004°
Longitude
33.1175°
Altitude
587.349 km
Speed
7.571 km/s
True Right ascension
15h 34m 21s
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
02:55:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
602.118 km
Perigee altitude
585.44 km
Semi-major axis
6,971.916 km
Eccentricity
0.0012
Inclination
49.9861°
RAAN
233.5897°
Arg. of periapsis
318.2053°
True anomaly
41.88895°
Mean anomaly
41.7975°
Eccentric anomaly
41.84322°
Mean motion
3.72834 °/min
Orbital period
96.56 mins
BSTAR
0.00034979
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
|