GEESAT 4-08, 65126
Orbit data source: Space-Track
GEESAT 4-08, 65126 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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65126 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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 GEESAT 4-08
1 65126U 25170H 26155.31109952 .00001768 00000-0 24722-3 0 9996
2 65126 49.9646 186.9274 0021408 291.5806 68.2850 14.82118312 45147Epoch: 2026-06-04T07:27Z
TLE epoch observation values (Epoch: 2026-06-04T07:27:58.998Z)
Latitude
-0.00003°
Longitude
-177.82564°
Altitude
617.668 km
Speed
7.554 km/s
True Right ascension
12h 27m 42s
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
11:53:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.398 km
Perigee altitude
608.42 km
Semi-major axis
7,001.546 km
Eccentricity
0.00214
Inclination
49.9646°
RAAN
186.9274°
Arg. of periapsis
291.5806°
True anomaly
68.51313°
Mean anomaly
68.285°
Eccentric anomaly
68.39904°
Mean motion
3.70469 °/min
Orbital period
97.17 mins
BSTAR
0.00024722
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Other satellites on launch #170 in the year 2025 (2025-08-08 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 4-08 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 | 2026-06-08 03:53:23.718Z | 226.756° WSW | 2026-06-08 03:56:23.718Z | 191.332° SSW | 43.096° | 2026-06-08 04:00:23.718Z | 59.479° ENE |
| 6 mins | 2026-06-08 05:36:23.718Z | 294.661° NW | 2026-06-08 05:38:23.718Z | 335.235° NNW | 27.765° | 2026-06-08 05:42:23.718Z | 43.432° NE |
| 5 mins | 2026-06-08 07:19:23.718Z | 330.563° NNW | 2026-06-08 07:21:23.718Z | 7.45° NNE | 21.505° | 2026-06-08 07:24:23.718Z | 52.332° ENE |
| 7 mins | 2026-06-08 09:00:23.718Z | 319.558° NNW | 2026-06-08 09:03:23.718Z | 16.871° NNE | 32.989° | 2026-06-08 09:07:23.718Z | 91.392° ESE |
| 7 mins | 2026-06-08 10:42:23.718Z | 286.801° WNW | 2026-06-08 10:45:23.718Z | 211.362° SW | 36.747° | 2026-06-08 10:49:23.718Z | 147.779° 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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