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
Taizhou Xingkong
Mission
Operational spacecraft
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GEESAT 4-08
1 65126U 25170H 25283.38041274 .00004004 00000-0 47101-3 0 9998
2 65126 49.9741 252.6152 0008152 306.2142 53.8043 14.86707830 9335Epoch: 2025-10-10T09:07Z
TLE epoch observation values (Epoch: 2025-10-10T09:07:47.660Z)
Latitude
-0.00004°
Longitude
96.4395°
Altitude
605.412 km
Speed
7.56 km/s
True Right ascension
16h 50m 27s
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
19:15:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.69 km
Perigee altitude
603.298 km
Semi-major axis
6,987.131 km
Eccentricity
0.00082
Inclination
49.9741°
RAAN
252.6152°
Arg. of periapsis
306.2142°
True anomaly
53.87973°
Mean anomaly
53.8043°
Eccentric anomaly
53.84201°
Mean motion
3.71616 °/min
Orbital period
96.87 mins
BSTAR
0.00047101
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-11 01:27:16.862Z | 242.593° WSW | 2025-10-11 01:31:16.862Z | 293.281° NW | 43.162° | 2025-10-11 01:35:16.862Z | 51.937° ENE |
| 5 mins | 2025-10-11 03:11:16.862Z | 307.398° NW | 2025-10-11 03:13:16.862Z | 346.505° N | 23.878° | 2025-10-11 03:16:16.862Z | 38.044° NE |
| 5 mins | 2025-10-11 04:53:16.862Z | 327.72° NNW | 2025-10-11 04:55:16.862Z | 2.584° NNE | 21.885° | 2025-10-11 04:58:16.862Z | 54.258° ENE |
| 7 mins | 2025-10-11 06:34:16.862Z | 315.433° NNW | 2025-10-11 06:37:16.862Z | 18.569° NNE | 38.54° | 2025-10-11 06:41:16.862Z | 103.935° ESE |
| 6 mins | 2025-10-11 08:16:16.862Z | 270.78° WNW | 2025-10-11 08:18:16.862Z | 230.141° WSW | 27.041° | 2025-10-11 08:22:16.862Z | 164.088° S |
| 6 mins | 2025-10-12 00:01:16.862Z | 194.381° SSW | 2025-10-12 00:04:16.862Z | 123.977° SE | 31.244° | 2025-10-12 00:07:16.862Z | 73.348° 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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