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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GEESAT 4-10
1 65128U 25170K 26095.87898944 .00003048 00000-0 39029-3 0 9997
2 65128 49.9789 101.7921 0032211 8.6292 351.5193 14.83597280 36336Epoch: 2026-04-05T21:05Z
TLE epoch observation values (Epoch: 2026-04-05T21:05:44.687Z)
Latitude
-0.00006°
Longitude
-48.82223°
Altitude
596.248 km
Speed
7.575 km/s
True Right ascension
06h 47m 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
13:38:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.292 km
Perigee altitude
596.216 km
Semi-major axis
6,996.891 km
Eccentricity
0.00322
Inclination
49.9789°
RAAN
101.7921°
Arg. of periapsis
8.6292°
True anomaly
351.46465°
Mean anomaly
351.5193°
Eccentric anomaly
351.492°
Mean motion
3.70839 °/min
Orbital period
97.08 mins
BSTAR
0.00039029
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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 | 2026-04-06 08:51:31.856Z | 312.092° NW | 2026-04-06 08:55:31.856Z | 19.805° NNE | 36.83° | 2026-04-06 08:59:31.856Z | 100.063° ESE |
| 6 mins | 2026-04-06 10:34:31.856Z | 276.697° WNW | 2026-04-06 10:36:31.856Z | 237.854° WSW | 29.695° | 2026-04-06 10:40:31.856Z | 161.661° S |
| 5 mins | 2026-04-07 02:22:31.856Z | 183.368° SSW | 2026-04-07 02:24:31.856Z | 136.257° SSE | 29.425° | 2026-04-07 02:27:31.856Z | 77.981° E |
| 6 mins | 2026-04-07 04:03:31.856Z | 270.595° WNW | 2026-04-07 04:05:31.856Z | 319.853° NNW | 36.237° | 2026-04-07 04:09:31.856Z | 46.086° ENE |
| 6 mins | 2026-04-07 05:45:31.856Z | 311.119° NW | 2026-04-07 05:47:31.856Z | 344.085° N | 21.15° | 2026-04-07 05:51:31.856Z | 46.655° ENE |
| 5 mins | 2026-04-07 07:28:31.856Z | 335.748° NNW | 2026-04-07 07:30:31.856Z | 17.182° NNE | 24.915° | 2026-04-07 07:33:31.856Z | 67.869° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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