GEESAT 6-11, 65723
Orbit data source: Space-Track
GEESAT 6-11, 65723 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.
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65723 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.1 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GEESAT 6-11
1 65723U 25214M 26171.37058256 .00001234 00000-0 17625-3 0 9994
2 65723 49.9848 293.1746 0010337 235.2484 124.7481 14.83375469 39987Epoch: 2026-06-20T08:53Z
TLE epoch observation values (Epoch: 2026-06-20T08:53:38.333Z)
Latitude
-0.00003°
Longitude
-108.82132°
Altitude
623.359 km
Speed
7.546 km/s
True Right ascension
19h 32m 41s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:12:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.684 km
Perigee altitude
612.217 km
Semi-major axis
6,997.587 km
Eccentricity
0.00103
Inclination
49.9848°
RAAN
293.1746°
Arg. of periapsis
235.2484°
True anomaly
124.84536°
Mean anomaly
124.7481°
Eccentric anomaly
124.79674°
Mean motion
3.70784 °/min
Orbital period
97.09 mins
BSTAR
0.00017625
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Other satellites on launch #214 in the year 2025 (2025-09-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 6-11 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 10:57:56.870Z | 225.122° WSW | 2026-06-21 11:00:56.870Z | 95.374° ESE | 43.16° | 2026-06-21 11:04:56.870Z | 58.49° ENE |
| 6 mins | 2026-06-21 12:39:56.870Z | 293.213° NW | 2026-06-21 12:41:56.870Z | 332.189° NNW | 27.422° | 2026-06-21 12:45:56.870Z | 42.607° NE |
| 5 mins | 2026-06-21 14:22:56.870Z | 330.27° NNW | 2026-06-21 14:24:56.870Z | 7.082° NNE | 21.166° | 2026-06-21 14:27:56.870Z | 52.174° ENE |
| 7 mins | 2026-06-21 16:03:56.870Z | 320.244° NNW | 2026-06-21 16:06:56.870Z | 19.835° NNE | 32.629° | 2026-06-21 16:10:56.870Z | 91.78° ESE |
| 6 mins | 2026-06-21 17:45:56.870Z | 285.648° WNW | 2026-06-21 17:48:56.870Z | 202.942° SW | 36.139° | 2026-06-21 17:51:56.870Z | 151.01° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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