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: 4 days ago
TLE from 4 days ago
0 GEESAT 4-10
1 65128U 25170K 26155.28016901 .00001753 00000-0 24559-3 0 9997
2 65128 49.9768 187.0786 0025682 241.9485 117.8854 14.82043725 45144Epoch: 2026-06-04T06:43Z
TLE epoch observation values (Epoch: 2026-06-04T06:43:26.602Z)
Latitude
-0.00007°
Longitude
-166.509°
Altitude
631.867 km
Speed
7.539 km/s
True Right ascension
12h 28m 18s
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
10:49:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.624 km
Perigee altitude
605.66 km
Semi-major axis
7,001.779 km
Eccentricity
0.00257
Inclination
49.9768°
RAAN
187.0786°
Arg. of periapsis
241.9485°
True anomaly
118.14513°
Mean anomaly
117.8854°
Eccentric anomaly
118.0153°
Mean motion
3.70451 °/min
Orbital period
97.18 mins
BSTAR
0.00024559
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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 | 2026-06-08 03:07:23.067Z | 195.838° SSW | 2026-06-08 03:10:23.067Z | 146.099° SSE | 29.504° | 2026-06-08 03:14:23.067Z | 73.926° E |
| 7 mins | 2026-06-08 04:49:23.067Z | 265.441° W | 2026-06-08 04:52:23.067Z | 343.954° N | 37.435° | 2026-06-08 04:56:23.067Z | 48.342° ENE |
| 5 mins | 2026-06-08 06:32:23.067Z | 315.731° NNW | 2026-06-08 06:34:23.067Z | 351.486° N | 22.417° | 2026-06-08 06:37:23.067Z | 40.447° NE |
| 6 mins | 2026-06-08 08:14:23.067Z | 325.776° NNW | 2026-06-08 08:17:23.067Z | 22.114° NNE | 25.183° | 2026-06-08 08:20:23.067Z | 69.259° E |
| 7 mins | 2026-06-08 09:56:23.067Z | 307.885° NW | 2026-06-08 09:59:23.067Z | 86.049° E | 44.059° | 2026-06-08 10:03:23.067Z | 121.141° SE |
| 4 mins | 2026-06-08 11:38:23.067Z | 257.592° W | 2026-06-08 11:40:23.067Z | 225.244° WSW | 17.801° | 2026-06-08 11:42:23.067Z | 195.017° SSW |
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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