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: 16 hours ago
TLE from 16 hours ago
0 GEESAT 4-10
1 65128U 25170K 26034.60311521 .00046542 00000-0 10279-2 0 9993
2 65128 49.9860 41.6343 0011829 342.1045 17.9500 15.43281150 27024Epoch: 2026-02-03T14:28Z
TLE epoch observation values (Epoch: 2026-02-03T14:28:29.154Z)
Latitude
-0.00001°
Longitude
50.73114°
Altitude
429.323 km
Speed
7.66 km/s
True Right ascension
02h 46m 32s
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
08:36:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.276 km
Perigee altitude
429.152 km
Semi-major axis
6,815.351 km
Eccentricity
0.00118
Inclination
49.986°
RAAN
41.6343°
Arg. of periapsis
342.1045°
True anomaly
17.99183°
Mean anomaly
17.95°
Eccentric anomaly
17.97091°
Mean motion
3.85754 °/min
Orbital period
93.32 mins
BSTAR
0.0010279
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-04 07:59:41.532Z | 333.013° NNW | 2026-02-04 08:01:41.532Z | 17.149° NNE | 21° | 2026-02-04 08:03:41.532Z | 61.725° ENE |
| 5 mins | 2026-02-04 09:37:41.532Z | 300.599° NW | 2026-02-04 09:39:41.532Z | 148.216° SSE | 43.272° | 2026-02-04 09:42:41.532Z | 128.407° SE |
| 5 mins | 2026-02-05 02:23:41.532Z | 190.646° SSW | 2026-02-05 02:25:41.532Z | 136.345° SSE | 27.593° | 2026-02-05 02:28:41.532Z | 73.718° E |
| 4 mins | 2026-02-05 04:01:41.532Z | 289.863° WNW | 2026-02-05 04:02:41.532Z | 323.513° NNW | 30.167° | 2026-02-05 04:05:41.532Z | 39.982° NE |
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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