GEESAT 4-10, 65128
Orbit data source: Space-Track
GEESAT 4-10, 65128 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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65128 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: 23 hours ago
TLE from 23 hours ago
0 GEESAT 4-10
1 65128U 25170K 26225.19202503 .00000511 00000-0 91318-4 0 9999
2 65128 49.9769 223.6726 0024401 150.1413 210.0922 14.82324615 55510Epoch: 2026-08-13T04:36Z
TLE epoch observation values (Epoch: 2026-08-13T04:36:30.962Z)
Latitude
-0.00003°
Longitude
-167.09158°
Altitude
637.326 km
Speed
7.533 km/s
True Right ascension
14h 54m 41s
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
17:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.841 km
Perigee altitude
605.675 km
Semi-major axis
7,000.895 km
Eccentricity
0.00244
Inclination
49.9769°
RAAN
223.6726°
Arg. of periapsis
150.1413°
True anomaly
209.95237°
Mean anomaly
210.0922°
Eccentric anomaly
210.02225°
Mean motion
3.70521 °/min
Orbital period
97.16 mins
BSTAR
0.000091318
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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 4-10 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 | 2026-08-14 03:28:20.708Z | 250.343° W | 2026-08-14 03:32:20.708Z | 349.514° N | 41.092° | 2026-08-14 03:36:20.708Z | 50.856° ENE |
| 5 mins | 2026-08-14 05:12:20.708Z | 313.572° NW | 2026-08-14 05:14:20.708Z | 352.452° N | 22.874° | 2026-08-14 05:17:20.708Z | 40.597° NE |
| 6 mins | 2026-08-14 06:54:20.708Z | 327.234° NNW | 2026-08-14 06:56:20.708Z | 1.63° NNE | 22.598° | 2026-08-14 07:00:20.708Z | 65.945° ENE |
| 6 mins | 2026-08-14 08:36:20.708Z | 315.574° NNW | 2026-08-14 08:39:20.708Z | 64.407° ENE | 40.354° | 2026-08-14 08:42:20.708Z | 109.65° ESE |
| 5 mins | 2026-08-14 10:18:20.708Z | 260.144° W | 2026-08-14 10:20:20.708Z | 220.417° SW | 22.294° | 2026-08-14 10:23:20.708Z | 174.979° S |
| 7 mins | 2026-08-15 02:05:20.708Z | 209.584° SW | 2026-08-15 02:08:20.708Z | 147.026° SSE | 37.859° | 2026-08-15 02:12:20.708Z | 66.018° ENE |
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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