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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GEESAT 4-10
1 65128U 25170K 25330.62393961 .00016168 00000-0 77646-3 0 9994
2 65128 49.9989 31.0990 0009392 81.4141 278.7876 15.18897285 16383Epoch: 2025-11-26T14:58Z
TLE epoch observation values (Epoch: 2025-11-26T14:58:28.382Z)
Latitude
-0.00001°
Longitude
100.6882°
Altitude
508.742 km
Speed
7.612 km/s
True Right ascension
02h 04m 23s
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
04:32:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.412 km
Perigee altitude
503.473 km
Semi-major axis
6,888.079 km
Eccentricity
0.00094
Inclination
49.9989°
RAAN
31.099°
Arg. of periapsis
81.4141°
True anomaly
278.68122°
Mean anomaly
278.7876°
Eccentric anomaly
278.73441°
Mean motion
3.79661 °/min
Orbital period
94.82 mins
BSTAR
0.00077646
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-28 08:16:45.919Z | 278.484° WNW | 2025-11-28 08:19:45.919Z | 330.01° NNW | 25.374° | 2025-11-28 08:22:45.919Z | 35.214° NE |
| 5 mins | 2025-11-28 11:37:45.919Z | 333.074° NNW | 2025-11-28 11:39:45.919Z | 20.307° NNE | 25.835° | 2025-11-28 11:42:45.919Z | 79.143° E |
| 5 mins | 2025-11-28 13:16:45.919Z | 292.035° WNW | 2025-11-28 13:18:45.919Z | 232.351° WSW | 41.126° | 2025-11-28 13:21:45.919Z | 140.631° SSE |
| 6 mins | 2025-11-29 06:19:45.919Z | 221.264° SW | 2025-11-29 06:21:45.919Z | 176.506° S | 42.033° | 2025-11-29 06:25:45.919Z | 60.156° 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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