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: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-08
1 65126U 25170H 26289.26556621 .00001512 00000-0 21412-3 0 9997
2 65126 49.9659 287.0683 0020138 86.4058 273.9182 14.82447654 65012Epoch: 2026-10-16T06:22Z
TLE epoch observation values (Epoch: 2026-10-16T06:22:24.920Z)
Latitude
-0.00002°
Longitude
166.67539°
Altitude
621.214 km
Speed
7.55 km/s
True Right ascension
19h 08m 16s
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
09:12:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.47 km
Perigee altitude
608.275 km
Semi-major axis
7,000.509 km
Eccentricity
0.00201
Inclination
49.9659°
RAAN
287.0683°
Arg. of periapsis
86.4058°
True anomaly
273.68794°
Mean anomaly
273.9182°
Eccentric anomaly
273.80307°
Mean motion
3.70552 °/min
Orbital period
97.15 mins
BSTAR
0.00021412
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-17 01:56:37.240Z | 188.011° SSW | 2026-10-17 01:59:37.240Z | 137.375° SSE | 28.4° | 2026-10-17 02:02:37.240Z | 82.93° E |
| 7 mins | 2026-10-17 03:37:37.240Z | 255.542° W | 2026-10-17 03:40:37.240Z | 308.503° NW | 54.016° | 2026-10-17 03:44:37.240Z | 47.425° ENE |
| 6 mins | 2026-10-17 05:20:37.240Z | 306.682° NW | 2026-10-17 05:23:37.240Z | 0.494° NNE | 23.627° | 2026-10-17 05:26:37.240Z | 44.011° NE |
| 5 mins | 2026-10-17 07:03:37.240Z | 332.343° NNW | 2026-10-17 07:05:37.240Z | 10.239° NNE | 25.528° | 2026-10-17 07:08:37.240Z | 61.74° ENE |
| 7 mins | 2026-10-17 08:44:37.240Z | 310.957° NW | 2026-10-17 08:47:37.240Z | 17.716° NNE | 67.743° | 2026-10-17 08:51:37.240Z | 114.106° SE |
| 5 mins | 2026-10-17 10:26:37.240Z | 266.442° W | 2026-10-17 10:28:37.240Z | 233.032° WSW | 22.197° | 2026-10-17 10:31:37.240Z | 183.554° SSW |
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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