GEESAT 4-06, 65124
Orbit data source: Space-Track
GEESAT 4-06, 65124 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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65124 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, 0.9 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 GEESAT 4-06
1 65124U 25170F 26225.17281294 .00000525 00000-0 89237-4 0 9999
2 65124 49.9840 269.7518 0019126 259.9376 99.9404 14.84193866 54893Epoch: 2026-08-13T04:08Z
TLE epoch observation values (Epoch: 2026-08-13T04:08:51.038Z)
Latitude
-0.00003°
Longitude
-114.07708°
Altitude
618.994 km
Speed
7.549 km/s
True Right ascension
17h 59m 00s
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
17:52:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.257 km
Perigee altitude
603.5 km
Semi-major axis
6,995.015 km
Eccentricity
0.00191
Inclination
49.984°
RAAN
269.7518°
Arg. of periapsis
259.9376°
True anomaly
100.15619°
Mean anomaly
99.9404°
Eccentric anomaly
100.0483°
Mean motion
3.70988 °/min
Orbital period
97.04 mins
BSTAR
0.000089237
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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 4-06 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 | 2026-08-14 04:31:45.948Z | 175.004° S | 2026-08-14 04:34:45.948Z | 132.777° SE | 18.116° | 2026-08-14 04:37:45.948Z | 88.881° E |
| 7 mins | 2026-08-14 06:12:45.948Z | 241.301° WSW | 2026-08-14 06:15:45.948Z | 319.053° NNW | 44.497° | 2026-08-14 06:19:45.948Z | 53.606° ENE |
| 6 mins | 2026-08-14 07:54:45.948Z | 294.933° NW | 2026-08-14 07:57:45.948Z | 347.885° N | 24.951° | 2026-08-14 08:00:45.948Z | 38.548° NE |
| 6 mins | 2026-08-14 09:37:45.948Z | 326.083° NNW | 2026-08-14 09:39:45.948Z | 359.823° N | 21.955° | 2026-08-14 09:43:45.948Z | 61.171° ENE |
| 6 mins | 2026-08-14 11:19:45.948Z | 321.719° NNW | 2026-08-14 11:21:45.948Z | 4.398° NNE | 36.624° | 2026-08-14 11:25:45.948Z | 99.759° ESE |
| 6 mins | 2026-08-14 13:00:45.948Z | 278.663° WNW | 2026-08-14 13:03:45.948Z | 216.664° SW | 29.058° | 2026-08-14 13:06:45.948Z | 165.155° S |
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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