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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Edit Public Description
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: 2 days ago
TLE from 2 days ago
0 GEESAT 4-08
1 65126U 25170H 25330.26462788 .00017008 00000-0 82532-3 0 9990
2 65126 49.9755 32.3768 0010645 250.8864 109.0937 15.18487880 16331Epoch: 2025-11-26T06:21Z
TLE epoch observation values (Epoch: 2025-11-26T06:21:03.848Z)
Latitude
0.00002°
Longitude
-128.3276°
Altitude
513.365 km
Speed
7.607 km/s
True Right ascension
02h 09m 30s
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
04:34:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.518 km
Perigee altitude
503.85 km
Semi-major axis
6,889.321 km
Eccentricity
0.00106
Inclination
49.9755°
RAAN
32.3768°
Arg. of periapsis
250.8864°
True anomaly
109.20892°
Mean anomaly
109.0937°
Eccentric anomaly
109.15132°
Mean motion
3.79558 °/min
Orbital period
94.85 mins
BSTAR
0.00082532
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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 | 2025-11-28 07:31:50.896Z | 257.547° W | 2025-11-28 07:34:50.896Z | 315.154° NNW | 36.722° | 2025-11-28 07:38:50.896Z | 47.711° ENE |
| 4 mins | 2025-11-28 09:12:50.896Z | 314.133° NW | 2025-11-28 09:14:50.896Z | 352.362° N | 19.157° | 2025-11-28 09:16:50.896Z | 29.703° NE |
| 5 mins | 2025-11-28 10:52:50.896Z | 333.577° NNW | 2025-11-28 10:54:50.896Z | 13.384° NNE | 20.285° | 2025-11-28 10:57:50.896Z | 63.615° ENE |
| 6 mins | 2025-11-28 12:31:50.896Z | 314.464° NW | 2025-11-28 12:33:50.896Z | 353.202° N | 39.61° | 2025-11-28 12:37:50.896Z | 111.578° ESE |
| 4 mins | 2025-11-28 14:11:50.896Z | 251.236° W | 2025-11-28 14:12:50.896Z | 230.453° WSW | 19.35° | 2025-11-28 14:15:50.896Z | 178.784° S |
| 5 mins | 2025-11-29 05:35:50.896Z | 182.437° SSW | 2025-11-29 05:37:50.896Z | 135.313° SSE | 26.232° | 2025-11-29 05:40:50.896Z | 77.893° E |
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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