GEESAT 6-06, 65718
Orbit data source: Space-Track
GEESAT 6-06, 65718 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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65718 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 6-06
1 65718U 25214G 26171.39181417 .00001041 00000-0 15375-3 0 9992
2 65718 49.9919 291.2825 0010238 249.2693 110.7148 14.83139851 40018Epoch: 2026-06-20T09:24Z
TLE epoch observation values (Epoch: 2026-06-20T09:24:12.744Z)
Latitude
-0.00001°
Longitude
-118.37771°
Altitude
622.514 km
Speed
7.547 km/s
True Right ascension
19h 25m 07s
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
07:12:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.355 km
Perigee altitude
613.025 km
Semi-major axis
6,998.327 km
Eccentricity
0.00102
Inclination
49.9919°
RAAN
291.2825°
Arg. of periapsis
249.2693°
True anomaly
110.82448°
Mean anomaly
110.7148°
Eccentric anomaly
110.76965°
Mean motion
3.70725 °/min
Orbital period
97.11 mins
BSTAR
0.00015375
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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 6-06 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 09:48:59.074Z | 183.355° SSW | 2026-06-21 09:51:59.074Z | 132.436° SE | 24.007° | 2026-06-21 09:54:59.074Z | 82.91° E |
| 7 mins | 2026-06-21 11:29:59.074Z | 253.589° W | 2026-06-21 11:32:59.074Z | 320.768° NNW | 41.068° | 2026-06-21 11:36:59.074Z | 49.394° ENE |
| 6 mins | 2026-06-21 13:12:59.074Z | 309.08° NW | 2026-06-21 13:14:59.074Z | 344.805° N | 22.939° | 2026-06-21 13:18:59.074Z | 45.985° ENE |
| 6 mins | 2026-06-21 14:54:59.074Z | 323.778° NNW | 2026-06-21 14:57:59.074Z | 16.779° NNE | 23.247° | 2026-06-21 15:00:59.074Z | 63.443° ENE |
| 7 mins | 2026-06-21 16:36:59.074Z | 313.679° NW | 2026-06-21 16:39:59.074Z | 46.556° ENE | 41.863° | 2026-06-21 16:43:59.074Z | 112.376° ESE |
| 5 mins | 2026-06-21 18:18:59.074Z | 263.194° W | 2026-06-21 18:20:59.074Z | 225.813° WSW | 22.517° | 2026-06-21 18:23:59.074Z | 177.956° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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