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: 7 hours ago
TLE from 7 hours ago
0 GEESAT 4-10
1 65128U 25170K 26289.29856061 .00001644 00000-0 22987-3 0 9997
2 65128 49.9781 287.0418 0024574 34.3142 325.9377 14.82487070 65021Epoch: 2026-10-16T07:09Z
TLE epoch observation values (Epoch: 2026-10-16T07:09:55.636Z)
Latitude
-0.00006°
Longitude
154.73836°
Altitude
607.79 km
Speed
7.564 km/s
True Right ascension
19h 08m 10s
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
09:11:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.449 km
Perigee altitude
605.043 km
Semi-major axis
7,000.383 km
Eccentricity
0.00246
Inclination
49.9781°
RAAN
287.0418°
Arg. of periapsis
34.3142°
True anomaly
325.77958°
Mean anomaly
325.9377°
Eccentric anomaly
325.85868°
Mean motion
3.70562 °/min
Orbital period
97.15 mins
BSTAR
0.00022987
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-17 02:46:12.960Z | 220.089° SW | 2026-10-17 02:49:12.960Z | 130.043° SE | 66.579° | 2026-10-17 02:53:12.960Z | 60.542° ENE |
| 6 mins | 2026-10-17 04:28:12.960Z | 287.154° WNW | 2026-10-17 04:31:12.960Z | 351.774° N | 32.261° | 2026-10-17 04:34:12.960Z | 40.785° NE |
| 5 mins | 2026-10-17 06:11:12.960Z | 325.278° NNW | 2026-10-17 06:13:12.960Z | 0.359° NNE | 22.24° | 2026-10-17 06:16:12.960Z | 47.83° ENE |
| 6 mins | 2026-10-17 07:53:12.960Z | 327.673° NNW | 2026-10-17 07:55:12.960Z | 7.997° NNE | 35.612° | 2026-10-17 07:59:12.960Z | 85.94° E |
| 7 mins | 2026-10-17 09:34:12.960Z | 292.509° NW | 2026-10-17 09:37:12.960Z | 224.529° SW | 56.129° | 2026-10-17 09:41:12.960Z | 143.614° 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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